PITTSBURGH MINING AND SAFETY RESEARCH CENTER …PITTSBURGH MINING AND SAFETY RESEARCH CENTER INTERIM...

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Interim Report No. 1646

March 22, 1974

BUREAU OF MINES. PITTSBURGH. PA.,_

R(P_00CEOBY

• NATIONAL TECHNICAL 'INFORMATION SERVICE

U.S.DEPARTMENTOFCOMMERCESPRINGFIELD.VA.22161

UNITED STATE._DEPARTMENT Ol_

THE INTERIOR

https://ntrs.nasa.gov/search.jsp?R=19740020114 2020-02-10T05:08:59+00:00Z

PITTSBURGH MINING AND SAFETY RESEARCH CENTER

INTERIM REPORT NO. 1646

THE HARD START PHENOMENA IN HYPERGOLIC ENGINES

VOLUME I. BIBLIOGRAPHY

By

Yael Miron and H. E. Perlee

APPROVED:

Robert W. Van Dolah

Research Director

Pittsburgh Mining and

Safety Research Center

U. S. Department of the Interior

Bureau of Mines

Pittsburgh, Pennsylvania 15213

March 22, 1974

THEHARDSTARTPHENOMENAIN HYPERGOLICENGINES

VOLUMEI. BIBLIOGRAPHY

by

Yael Miron and H. E. Perlee

Prepared for

Manned Spacecraft Center

National Aeronautics and Space Administration

Houston, Texas

Order No. T-39882(G)

UNITED STATES DEPARTMENT OF THE INTERIOR

BUREAU OF MINES

//

PREFACE

This bibliography contains information deemed important to the hard start

phenomenon in the Apollo attitude Control RSC engine program. It was compiled

after an exhaustive study and critical evaluation of the literature.

Some of the references in the subsequent volumes of this report are

repeated in the bibliography. The bibliography spans a 20-year period ending

in early 1970.

///

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THE HARD START PHENOMENA IN HYPERGOLIC ENGINES

VOLUME I. BIBLIOGRAPHY

by

Yael Miron I and H. E. Perlee 2

ACKNOWLEDGMENT

The authors want to acknowledge the effort contributed to this research

by Messrs. Theodore Christos, Harry K. James, and Glen Reid, and the technical

support supplied by Messrs. Bernard Rosenbaum and Carl Hohmann of the Manned

Spacecraft Cente_ Houston, Texas.

iChemical research engineer.

2Chief, Technical Support.

Both authors are with the Pittsburgh Mining and Safety Research Center,

Bureau of Mines, U.S. Department of the Interior, Pittsburgh, Pa.

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BIBLIOGRAPHY 3

Abbe, C. J., C. W. McLaughlin, and R. R. Weiss. Influence of Storable

Propellant Liquid Rocket Design Parameters on Combustion Instability.

J. Spacecraft, v. 5, No. 5, May 1968, pp. 584-589.

Influence of Storable Propellant Liquid Rocket Design Parameters

on Combustion Instability. Air Force Rocket Propulsion Lab., Air Force

Report No. AFRPL-TR-69-14, Systems Command, Edwards, Calif., January 1969.

Adams, G. K., and G. B. Cook. The Effect of Pressure on the Mechanism

and Speed of the Hydrazine Decomposition Flame. Combustion and Flame,

v. 4, March 1960, pp. 9-18.

Adams, G. K., and G. W. Stocks. The Combustion of Hydrazine. 4th Sympo-

sium (International) on Combustion, Paper 26, at the Massachusetts

Institute of Technology, Cambridge, Mass., Sept. 1-5, 1952, pp. 239-248.

Pub. by Williams and Wilkins Company, Baltimore, 1953.

Addison, C. C., and J. Lewis. The Chemistry of the Nitrosyl Group (NO).

Chem. S,c. Quart. Reviews, v. 9, 1955, pp. 115-149.

Adelman, Barnet R. Apparatus for Laboratory-Scale Determination of Igni-

tion Lag of Spontaneous Liquid Rocket Propellants. Jet Propulsion Lab.,

California Institute of Technology, Progress Rept. No. PR-9-52,

Feb. 23, 1951. Dept. of the Army, Ordnance Corps (contract

No. DA-04-495-ORD 18), ORDCIT Project.

7. Ignition-Lag Characterzstics of Some Hydrazine-Nitric Acid Pro-

pellant Systems. Jet Propuh_ion Lab., California Institute of Technol-

ogy, Pasadena, Calif., Progress Rept. No. 20-164, Jan. 29, 1952. Dept.

of the Army, Ordnance Corps (contract No. DA-04-495-ORD 18), ORDCiT

Project.

A Study of Ignition-Lag Characteristics of Some Liquid Rocket8. _is With Red Fuming Nitric Acid, Including Additives to the Oxidizer.

Jet Propulsion Lab., California Institute of Technology, Pasadena,

Calif., Progress Rept. No. PR-20-138, Apr. 18, 1951. Dept. of the Army,

Ordnance Corps (contract No. DA-04-495-ORD 18), ORDCIT Project.

9. Adler, J. A One-Dimensional Theory of Liquid-Fuel Rocket Combustion III:

The Effect of Non-Uniform Droplet Radii, Injection Velocities and

Physical Properties. Imperial College of Science and Engineering,

Englan¢ Aeronautical Res. Council, Rept. No. ARC-20,830; C.F. 466,

Feb. 18, 1959, 15 pp.

I0. Adler, J., and Julius W. Enig. The Critical Conditions in Thermal Explo-

sion Theory With Reactant Consumption. Imperial College of Science and

Technology, Dept. of Mathematics_ Univ. of London, England, Dec. 31,

1963. U.S. Naval Ordnance Lab., White Oak, Silver Spring, Md. (Task

No. R360-FR-105-59). Report No. NOL-TR-63-251.

/

3Titles enclosed in parentheses are translations from the language in which

the item was published.

i

II.

12.

13.

14.

!5.

16.

17.

18.

19.

20.

21.

22.

Adrian, R. C., and H. C. Edgington. Prototype Propellant-Testing System

Phases I and li--Feasibility Study and Preliminary Design. Aerojet-

General Corporation, Azusa, Calif., Chem. Products Div., Rept. No. 2452,

February 1963. Rocket Propulsion Lab., Res. and Tech. Div., Air Force

Systems Command, Edwards, Calif. Tech. Documentary Rept.

No. RTD-TDR-63-3 (contract No. AF04(611)-8196).

Africano, A. Maxin_am-Rate Theory of Impact Sensitivity. Proc. of the

1959 Cryogenic Engineering Conf., Univ. of California, Berkeley, Calif.,

Sept. 2-4, 1959. Advances in Cryogenic Engineering, v. 5, pp. 533-548.

Pub. by Plenum Press, Inc., New York, 1960.

Agosta, Vito D., Sanford S. Hammer, and William T. Peschke. High Fre-

quency Combustion Instability and Scaling of Liquid Rocket Propellant

Motors. First ICRPG Combustion Instability Conf., at the Polytechnic

Inst. of Brooklyn, November 1964.

Agosta, Vito D., and George Kraus. An Investigation of the Impulse Bit

Developed by a Pulsed Liquid Propellant Rocket Engine. Chem. Eng. Pro-

gress Symposium Series; Aerospace Techniques, v. 60, No. 52, 1964,

pp. 8-16.

Agoston, George A., Henry W_se, and Willis A. Rosser. Dynamic Factors

Affecting the Combustion cf Liquid Spheres. Jet Propulsion Lab.,

California Institute of Te.chnology, Progress Rept. No. 20-291, Nov. 20,

1956. Dept. of the Army.

Allen, Robert D. Thermal Conductivity of Gaseous Unsyr_netrical Dime=hyl-

hydrazine. AIAA J., v. i, July 1963, pp. 1689-1691.

Altman, David, and Barnet R. Adelman. Hybrid Rocket Motor Process Using

Solid and Liquid Phases. U.S. Pat. Office No. 3,234,729, assigned to

United Aircraft Corporation, East Hartford, Conn., Feb. 15, 1966.

Amster, Adolph B., and Joseph B. Levy. Solubility of Air, Ne and O_ in

n-Propyl Nitrate. A.R.S.J., v. 29, November 1959, pp. 870-871.

Anagnoustou, E., R. S. Brokaw, and J. N. Butler. Effect of Concentration

on Ignition Delays for Various Fuel-Oxygen-Nitrogen Migtures at Ele-

vated Temperatures. Report No. NACA-TN-3887. NACA, December 1956.

Andersen, W. H., and R. F. Chaiken. Application of Surface Decomposition

Kinetics to Detonation of Ar_nonlum Nitrate. A.R.S.J., v. 29, January

1959, pp. 49-51.

Andrews, F. C. On the Theory of Droplet Formation in One-Dimensional

Fluids. Physics Letter, v. 20_ No. I, .Jan. 15, 1966, pp. 17-19.

Andriankin, E. I., A. M. Kogan, A. S. Kompaneyets, and V. P. Kraynou

(Moscow). Propagation of Strong Explosion in Non-Homogeneous Atmos-

phere. Wright-Patterson AFB, Foreign Tech. Div., Transl. Rept.No. FTD-MT-63-228, 1963.

23.

24.

25.

26.

27.

28.

29.

30.

31.

32.

33.

Annand, Robert R., Ike Y. Chang, and R. M. Hurd. An Investigation ofPhysicochemical Methods for Detecting Toxic Propellants. Final Report.TRACOR,Incorporated, Austin, Tex. Aerospace Medical Res. Lab., Aero-space Medical Div., Air Force Systems Command,Wright-Patterson AirForce Base, Ohio. Tech. DocumentaryRept. No. AMRL-TDR-63-61(contractNo. AF 33(657)-8140), June 1963, 38 pp.

Antoine, Albert C. Effect of Pressure on Rate of Burning (DecompositionWith Flame) of Liquid Hydrazine. Report No. NASA-TN-D-2694. NASA,Lewis Research Center, March 1965.

Effect of Pressure on Rate of Burning (Decomposition With Flame)of Liquid Hydrazine. Combustion and Flame, v. I0, March 1966,

pp. 86-88.

The Effect of Some Additives on the Burning Rate of Liquid Hydra-

zine. Combustion and Flame, v. 6, December 1962, pp. 364-365.

The Mechanism of Burning of Liquid Hydrazine. 8th Symposium

(International) on Combustion, Paper No. II0, at the California Insti-

tute of Technology, Pasadena, Calif., Aug. 28-Sept. 3, 1960, pp. 1057-

1059. Pub. by Williams & Wilkins Company, Baltimore, Md., 1962.

Arakawa, Edward T., and Alvin H. Nielsen. Infrared Spectra and Molecular

Constants of NI_O_ and N16Om. J. of Molecular Spectroscopy, v. 2,

1958, pp. 413-427.

Arao, M., and B. R. Chandler. Feasibility Study for Development of a

Hypergolic Engine Space Power System. The Marquardt Corporation, Rept.No. TR-6076, NASA, Sept. 25, 1964.

Arenz, R. J., S.J. Projectile Size and Density Effects on Hypervelocity

Penetration. J. of Spacecraft, v. 6, No. ii, November 1969,pp. 1319-1321.

Armstrong, W. E., T. J. Jennings, and C. Z. Morgan. Hydrazine Nitrate

Catalyst Development. Shell Development Company--A Division of Shell

Oil Company, Emeryville, Calif., Rept. No. S-14083; 3 pp.; Quart. Rept.

No. 9, Nov. I, 1968-Jan. 31, 1969. Air Force Rocket Propulsion Lab.,

Res. and Tech. Div. (contract No. FO 4611-67-C-0023), Edwards AFB,Calif.

Arney, G. D., Jr., and A. B. Bailey. Effect of Temperature on Pressure

Measurements. AIAA J., v. i, No. 12, December 1963, pp/ 2863-2864.

Ashmore, P. G., and B. P. Levitt. The Thermal Reaction Between Hydrogen

and Nitrogen Dioxide. Part 4. Thermal Ignition of Hydrogen and Nitro-

gen Dioxide. Trans. of the Faraday Soc. (London), v. 54, 1958,pp. 390-393.

I! IJ IX U Lf U 14 !1 U u U H U a u c r.'

4

34.

35.

36.

37.

38.

39.

40.

41.

42.

43.

44.

45.

46.

Askey, Philip J. The Thermal Decomposition of Hydrazine. J. of the

American Chem. Soc., v. 52, 1930, pp. 970-974.

Aston, J. G., J. L. Wood, and T. P. Zolki. The Thermodynamic Properties

and Configuration of Unsymmetrical Dimethylhydrazine. J. of the Ameri-

can Chem. Soc., v. 75, 1953, pp. 6202-6204.

Audrieth, Ludwig F. Explosive Composition. (Assignor to) Olin Mathieson

Chemical Corp., U.S. Pat. 2,704,706, March 1955.

Parallelism in the Decomposition of Ammonium, Hydrazine, and

Hydroxylammonium Nitrites. Hyponitrous Acid as a Hydroxylamino Nitrous

Acid. J. of Phys. Chem., v. 34, 1930, pp. 538-542.

Audrieth, L. F., Betty Ackerson Ogg. The Chemistry of Hydrazine.

John Wiley & Sons, Inc., New York, 1951.

Avery, W. H. Space Heating Rates and High Temperature Kinetics. Fifth

Symposium (International) on Combustion Survey Paper No. X, at the

Univ. of _ittsburgh, Pittsburgh, Pa., Aug. 30-Sept. 3, 1954, pp. 86-9i.

Pub. by the Reinhold Publishing Corporation, New York, 1955 d Dept. ofthe Navy, Bureau of Ordnance (contract No. NOrd 7386).

Axworthy, A. E., J. M. Sullivan, S. Cohz, and E. Welz. Research on

Hydrazine Decomposition (Final Report). U.S. Air Force Rocket Propul-

sion Lab., Rocketdyne, A Div. of North American Rockwell Corporation,

Canoga Park, Calif., July 1969, 176 pp.

Bailey, T., R. Vandekoppel, G. Skartvedt, and T. Jefferson. Cryogenic

Propellant Stratification Analysis and Test Data Correlation. AIAA J.,

v. i, No. 7, July 1963, pp. 1657-1658.

Baker, Wilfred E., and Peter S. Westine.

Structures Using Dissimilar Materials.

pp. 951-959.

Modeling the Blast Response of

AIAA J., v. 7, No. 5, May 1969,

Bakhman, N. N. Increasing the Rate of Combustion by Introducing an Inert

Admixture. Doklady Akademij Nauk SSSR, v. 145, No. 6, 1962, 6 pp.

Wright-Patterson Air Force Base, Foreign Technology Div., Transl.,

Rept. No. FTD-TT-63-460.

Kinetic Combustion Conditions for Condensed Mixtures. Wright-

Patterson Air Force Base, Foreign Technology Div., Transl., Rept.

No. FTD-TT-61-298, Dec. 20, 1961.

Bamford, C. H. The Reaction Between Nitric Oxide and Some Nitrogenous

Free Radicals. Trans. of the Faraday Sot., v. 35, 1939, pp. 568-576.

Some New Observations on Hydrazine. Trans. of the Faraday Soc.,

_35, 1939, pp. 1239-1246.

H H Ill I1 11 11 11 1I ii 11 11 II 11 11 11 I1 i1 g E lg

47.

48.

49.

50.

51.

52.

53.

54.

55.

56.

57.

58.

Barr_re, M. Research in the Field of Chemical Propulsion. Chemical Pro-

pulsion Information Agency, pub. No. 67 (transl. by L. J. Holtschlog),

December 1964, 79 pp.

Barr_re, M., and J. J. Bernard. Influence of the Injector Pressure Drop

on Low Frequency Instability in Liquid Propellant Rockets. 6th Sympo-

sium (International) on Combustion, Paper No. 60, at Yale Univ., New

Haven, Conn., Aug. 19-24, 1956, pp. 487-492. Pub. by Reinhold Publish-

ing Corporation, New York, 1957.

Barr_re, M., and A. Moutet. Inflanmmtion and Ignition in Liquid-

Propellant Rocket Motors. Preprint of paper. 2nd AGARD Combustion

Colloquium, Liege, Belgium, Air Tech. Intelligence Center, U.S. Air

Force, Rept. No. ATIC-242044; also F-TS-8794/V, December 1955, 60 pp.

Barr_re, M., A. Moutet, and P. Sarrat. L'Evolution de la combustion dans

une chambre de fusee _ propergol liquide (Combustion Mechanism in a

Liquid Propellant Rocket Motor). Revue Generale des Sciences Appliques,

v. 3, 1957, pp. 313-333.

Barua, A. K., and T. K. Rai Dasidar. Force Constants of N204 and NOe and

Viscosity of the Dissociating System NsO4 _ 2NO_. J. of Chem. Phys.,

v. 43, Dec. I, 1965, pp. 4140-4142.

Basevich, V. Ya. On the Burning Velocity of Atomized Fuel. Moscow 1960,

Wright-Patterson Air Force Base, Foreign Tech. Div. Transl., Rept.

No. FTD-TT-62-1028.

Bauer, S. H., and M. R. Gustavson. Relaxation Techniques for Fast Reac-

tions. A Study of the Dissociation of Nitrogen Tetroxide. Discussions

of the Faraday Soc., v. 17, Jan. 28, 1954, pp. 69-90.

Baulknight, C. W. Comments on "Preigni=ion Phenomena in Small A-50/NTO

Pulsed Rocket Engines." J. of Spacecraft and Rockets_ v. 5, No. 8,

August 1968, p. 1008.

Baverle, George L., Robert C. Ahlert, and Jacob Silverman. Propellant

Compositions. U.S. Pat. No. 3,127,735, assigned to North American

Aviation, Apr. 7, 1964.

Beal, John L. Experimental Studies of Drop Breakup in Hypersonic Flow.

J. of Spacecraft and Rockets, v. 6, March 1969, p. 337.

Bellamy, L. J. The Infra-red Spectra of Complex Molecules. Ch. 17:

Nitro and Nitroso-Compounds) Nitrates and Nitrites, John Wiley & Sons,

Inc., 2nd ed., 1958, pp. 297-309.

Beltran, M. R., B. P. Breen, and M. Gerstein. Liquid Rocket Engine Com-

bustion Instability Studies. Dynamic Science Corporation, Monrovia,

Calif., Semiannual Rept. No. SN-68-SI, June 30, 1965. U.S. Air Force

Rocket Propulsion Laboratory (contract No. AF 04(611)-10542).

Ii II U U U U !/ U B 11 gl 11 11 11 il g £

59.

60.

61.

62.

63.

64.

65.

66.

67.

68.

69.

70.

Beltran, M. R., and N. A. Frankel. Prediction of Instability Zones in

Liquid Rocket Engines. AIAA J., v. 3, No. 3, March 1965, pp. 516-518.

Beltran, M. R., and R. O. Wright. A Non-Linear Model for Prediction of

Liquid Rocket Engine Instability. Dynamic Science Corporation,

Monrovia, Calif., NASA-U.S. AFRPL (contract No. NAS 7-366 and (par-

tially) contract No. AF 04(611)-10542), 3 pp.

Benson, A. M., and H. G. Drickamer. The Effect of Pressure on the Vibra-

tional Frequency of Bonds Containing Hydrogen. Discussions of the

Faraday Soc., v. 22, 1956, pp. 39-43.

Benson, G. M., M. M. Ei-Wakil, P. S. Myers, and O. A. Uyehara. A Fluo-

rescent Technique for Determining the Cross-Sectional Drop-Size Distri-

butions of Liquid Sprays. Paper No. 677-58, pres. at the ARS 13th Ann.

Meeting, Hotel Statler, New York, Nov. 17-21, 1958.

Berlad, A. L. Photochemical Effects on Explosive Instability. Combus-

tion and Flame (London), v. ii, 1967, pp. 445-452.

• Photochemical Processes in Explosion of NeH¢ and Related Com-

pounds. Defense Research Corporation, Santa Barbara, Calif., 2nd

Quart. Rept. No. CR-I09 28-2, March 1966. U.S. Air Force (contract

No. AF 04(611)-10928). Report No. AFRPL-TR-66-62.

Bernard, M. 1.. J. Dopes d'inflammation et de combustion pour systemes

utillses en autopropulsion (Additives To Promote Ignition and Combus-

tion of Propellants). French Pat. No. 1,063,439, assigned to

Laboratoire de Recherches Balistiques e= Aerodynamiques, May 3, 1954.

Surface Properties of Liquid Bipropellants and Their Effects on

the Kinetics of Ignition. Fifth Symposium (International) on Combus-

tion, Paper No. 14, at the Univ. of Pittsburgh, Pittsburgh, Pa.,

Aug. 30-Sept. 3, 1954, pp. 217-223. Pub. by Reinhold Publishing Corp.,1955.

Bernard, M. L. J., and J. Dufour. On the Existence of Detonation Condi-

tions in the Combustion of Some Nitric Acid Propellants. 8th Symposium(International) on Combustion, Paper No. 113, at the California Insti-

tute of Technology, Pasadena, Calif., Aug. 28-Sept. 3, 1960, pp. 1074-

1084. Pub. by Williams and Wilkins Company, Baltimore, Md., 1962.

Bibeler, Vernon H., J. L. Franklin, and Robert M. Reese. Electron Impact

Studies of Hydrazine and the Methyl-substituted Hydrazlnes. J. of the

American Chem. Soc., v. 81, 1959, pp. 68-73.

Bittker, David A. An Analytical Study of Turbulent and Molecular Mixingin Rocket Combustion. NACA-TN-4321, September 1958.

Effect of Ambient Air Velocity on Atomization of Two ImpingingWater Jets. NASA-TN-D-2087, February 1964.

71.

72.

73.

74.

75.

76.

77.

78.

79.

80.

81.

82.

Bittker, David A., and Richard S. Brokaw. Estimate of Chemical SpaceHeating Rates in Gas-PhaseCombustion With Application to RocketPropellants. A.R.S.J., v. 30, February 1960, pp. 179-185.

Bixson, L. L., and H. H. Deboi. Investigation of Rational Scaling Proce-dure for Liquid Fuel Rocket Engines. Sundstrand Corporation, Rept.No. SSD-TDR-62-78,June 1962, U.S. Air Force (contractNo. AF 18 (603)-107).

Bjerklie, J. W., and L. L. Bixson. The Experimental Determination ofChemical Conversion Times in Liquid Fuel Rocket Engines. SundstrandMachine Tool Co.,Mar. 15, 1958(U.S. Air Force Report No.AFOSR-TN-58-415).

Blacl_nan, A. W. Effect of Nonlinear Losses on the Design of Absorbersfor Combustion Instabilities. A.R.S.J., v. 30, 1960, pp. 1022-1028.

Blinov, V. I. Regularities Observed in Mixtures of Liquid Fuel DuringIgnition. Inzhenerno-Fizicheskiy Zhurnal, v. 4, No. 2, 1961. Wright-Patterson Air Force Base, Foreign Technology Div., Tech. Transl.Rept. No. FTD-TT-62-1037, September1962.

Boddington, T. The Growth and Decay Of Hot Spots and the RelationBetweenStructure and Stability. 9th Symposium(International) on Com-bustion, at Cornell Univ., Ithaca, N.Y., Aug. 27-Sept. i, 1962. Pub.by Academic Press, NewYork, 1963, pp. 287-293.

Bohme,D. K., and F. C. Fehsenfeld. Thermal Reactions of O_+ and O- ionsin GaseousAmmonia. Canadian J. of Chem., v. 47, No. !4, 1969,pp. 2715-2717.

Bolkhvitinov, L. G. The Probable Initiation Mechanismin the ExplosiveDecomposition of Liquids. Dokl. Akad. Nauk, SSSR,v. i26, No. 2, 1959,pp. 322-324.

Bollinger, Loren E. Experimental and Theoretical Investigation of theFluid Dynamicsof Rocket Combustion. Ohio State Univ., AeronauticalRes. Lab., Tech. Note No. ARL-TN-60-141, November1960. U.S. Air Force(contract No. AF 33(616)-5615).

Bollinger, Loren E., Michael C. Fong, JamesA. Laughrey, and Rudolph Edse.Experimental and Theoretical Studies on the Formation of DetonationWavesin Variable Geometry Tubes. Report No. NASA-TN-D-1983,June 1963.

Bollinger, L. E., J. R. Nicholson, J. O. KrisJansons, E. S. Fishburne,and R. Edse. Fluid Dynamics of Rocket Combustion. Ohio State Univ.Res. Foundation. Wright-Patterson Air Force Base, Ohio, AeronauticalRes. Lab., Rept. No. ARL-62-323 (contract No. AF 33(616)-5615), April1962, 104 pp.

Bonnell, John M. Commenton "Large-Amplitude Transverse Instability inRocket Motors." AIAA J., v. 7, No. 5, May 1969, p. 989.

83.

84.

85.

86.

87.

88.

89.

90.

91.

92.

93.

94.

95.

Borg, S. F. A Similarity Solution for a Blast in Free Space. J.Franklin Inst., supported by Republic Aviation Corp., Missiles SystemsDiv., as a subcontract for the Air Force Special WeaponsCenter AILDC(contract No. AF 29(601)-1028), December1959, pp. 446-452.

Borisov, A. A., S. M. Kogarko, and A. V. Lyubimov. Ignition of FuelFilms Behind ShockWavesin Air and Oxygen. Combustion and Flame,v. 12, October 1968, pp. 465-468.

Boudart, M. Rates of Evaporation of Liquids. Princeton Univ., ReportNo. AFOSR-464(contract No. AF 49(638)-32), March 1961.

Bowden,F. P. A Discussion on the Initiation and Growth of Explosionin Solids. Proc. of the Royal Soc. (London), Ser. A, Mathematicaland Phys. Sciences, v. 246, July 1958, pp. 145-167.

Bowden,F. P., and A. C. McLaren. Condition of Explosion of Azides.Effect of Size on Detonation Velocity. Nature, v. 175, No. 4458,Apr. 9, 1955, pp. 631-632.

Bowden, F. P., and M. P. McOnie. Formation of Cavities and Microjets inLiquids and Their Role in Initiation and Growth of Explosion. Proc. ofthe Royal Soo., Ser. A, v. 298 (1452), 1967, pp. 38-50.

Bowen, E. J., and A. W. Birley. The Vapour Phase Reaction BetweenHydra-zine and Oxygen. Trans. of the Faraday Soc., v. 47, 1951, pp. 580-583.

Boyn_on, Frederick P. Chemical Kinetic Analysis of Rocket Exhaust Tem-perature Measurements. AIAA J., v. 2, No. 3, March 1964, pp. 577-578.

Bragg, S. L. Changesin the Density and Temperature of Liquid Propel-lants in Rocket Engine Supply Systems. A.R.S.J., v. 29, September1959, pp. 672-674.

Branch, M. C., and R. F. Sawyer.Flow in Propellant Performance.1969, pp. 1322-1325.

Nonequilibrium Combustion and NozzleJ. Spacecraft, v. 6, No. Ii, November

Brandmaier, Harold E., John R. Dworschak, and L. A. Triggiani. Theoreti-cal Propellant Performance of Nitrogen Tetroxide-Unsymmetrical Dimeth-

ylhydrazine (NeO4-UDME). Curtiss-Wright Corp., Wright AeronauticalDiv., Nov. 9, 1960, 79 pp.

Bredfeldt, Hans R. Evaluation of a Light Scattering Technique for Deter-mining the Spray Characteristics of Impinging Liquid Jets. PrincetonUniv., Dept. of Aerospace and Mech. Science, NASA(grant No. NSG-99-60),Rept. No. TR-648, March 1964.

Breen, Bernard P. RandomWavePhenomena(Ignition Spiking and Popping)in Hypergolic Propellant Combustion. DynamicScience Corp., Monrovia,Calif., Monthly Status Rept. No. SN-87-3, NASA(contract No, NAS7-467),July II to Aug. i0, 1966.

Ii I/ i/ 11 1I U 11 I,I 11 I1 I1 11 11 11 11 11 ii g E lii

96.

97.

98.

99.

I00.

I0i.

102.

103.

104.

I05.

106.

107.

108.

Breen, B. P., and M. R. Beltran. Droplet Combustion in the Hyarazine-

Nitrogen Tetroxide System. Paper No. WSCI-65-21, pres. at the 1965

Fall Meeting of the Western States Section of the Combustion Inst.,

Oct. 25, 1965. U.S. Air Force (contract No. AF 04(611)-10542).

Breen, B. P., and B. R. Lawyer. Effects of Additives on the Combustion

of Hydrazine. Dynamic Science, a Div. of Marshall Industries,

Monrovia, Calif., First Quart. Re_t. No. SN-86-I-3 (May 2-Aug. 2,

1966). U.S. Air Force RPL (contract NO. AF 04(611)-I1616), September

1966. Report _. AFRPL-TR-66-254.

Effects of Additives on the Combustion of Hydrazine. Dynamic

Science, a Div. of Marshall Industries, Monrovia, Calif., Second

Quart. Rept. No. SN-86-6, Dec. I, 1966. U.S. Air Force Rocket Propul-

sion Lab. (contract No. AF 04(611)-11616).

Breen, B. P., L. B. Zung, B. R. Lawyer, T. C. Kosvic, and D. E. Coats.

Injection and Combustion of Hypergolic Propellants. Dynamic Science,

a Div. of Marshall Industries, Monrovia, Calif., Final Tech. Rept.

No. FO 4611-68-C-0040 (U.S. Air Force), April 1969, 90 pp. ReportNo. AFRPL-TR-69-48.

Brewer, Leroy, Jr., and Wheeler McGregor, Jr. Experimental Determina-

tion of a Rocket Exhaust Gas Temperature at Altitude by Infrared

Spectroscopy. Arnold Engineering Devel. Center, U.S. Air Force,

September 1961. Report No. AEDC-TN-61-94.

Brice, Donat B., and Norman Fishman. Some Physical Properties for the

System Nitrogen Tetroxide-Nitric Oxide. A.R.S.J., v. 29, 1959,pp. 354-357.

Brode, Harold L.

Charge of TNT.

Aug. 21, 1957.

A Calculation of the Blast Wave From a Spherical

Rand Corporation, Rept. No. RM-1965 (U.S. Air Force),

Blast Wave From a Spherical Charge. The Physics of Fluids, v. 2,

No. 2, March-April 1959, pp. 217-229.

Browne, A. W., and F. F. Shetterly. On the Oxidation of Hydrazine. I.

J. American Chem. Soc., v. 29, September 1907, pp. 1305-1312.

On the Oxidation of Hydrazine. II. J. American Chem. Soc.,

v. 30, January 1908, pp. 53-63.

On the Oxidation of Hydrazine. III. J. American Chem. Soc.,v. 31, February 1909, pp. 221-237.

On the Oxidation of Hydrazine. IV. J. American Chem. Soc.,v. 31, July 1909, pp. 783-799.

Bunion, C. A., and G. Stedman. Mechanism of the Azide-Nitrite Reaction.

Part III. Reaction in [$So] Water. J. of the Chem. Soc. (London),1959, pp. 3466-3474.

i0

109.

ii0.

ili.

112.

113.

114.

115.

116.

117.

118.

119.

Burgess, David, Joseph Grumer, and Michael G. Zabetakis. Research onthe Fire and Explosion Hazards Associated With NewLiquid Propellants.BuMinesProgress Rept. No. 3, for the period Nov. I, 1959-Jan. 31,1960, Office of Naval Res., Bureau of Ships Order NA onr-ll-60, 1960.

Research on the Fire and Explosion Hazards Associated With NewLiquid Propellants. BuMinesProgress Rept. No. 5, for period May i,1960, to July 31, 1960, Office of Naval Res., Bureau of Ships OrderNA-onr-ll-60, 1960.

Research on the Fire and Explosion Hazards Associated With NewLiquid Propellants. BuMines Progress Rept. No. 7, for the periodNov. I, 1960, to Jan. 31, 1961, Office of Naval Res., Bureau of ShipsOrder NA onr-ll-60, 1961.

Burgoyne, J. H. Mist and Spray Explosions. Chem.EnB. Progr., v. 53,No. 3, March 1957, pp. 121-M to 124-M.

Burke, Bernard A. A ProceduresManual for Computing Propellant Thermo-dynamic Properties. Naval OrdnanceLab., White Oak, Silver Spring,Md., Mar. 18, 1964. Report No. NOL-TR-63-202.

Burrows, G. Evaporation at Low Pressures. j, of Applied Chem., v. 7,July 7, 1957, pp. 375-384.

Burrows, Marshall C. DynamicResponseof Hydrazine-Nitrogen TetroxideCombustion to Transverse Gas Flow. NASA,Lewis Res. Center, Cleveland,Ohio, February 1969, 22 pp. Report No. NASATND-4984.

Mixing and Reaction Studies of Hydrazine and Nitrogen TetroxideUsing Photographic and Spectral Techniques. NASA,Lewis Res. Center,Cleveland, Ohio, June 1968, 22 pp. Report No. NASA-TND-4467.

Burstein, SamuelZ. Nonlinear Combustion Instability in Liquid-Propellant Rocket Engines. The Transverse Mode. I. The HydrodynamicDifferential and Difference Equations and Computer Algorith. Jet

Propulsion Lab., California Institute of Technology, Pasadena, Calif.,

Tech. Rept. No. 32-1111,NASA (contract No. NAS 7-100), Sept. 15, 1967.

Burstein, Samuel Z., and Vito D. Agosta. Combustion Instability Non-

Linear Analysis of Wave Propagation in a Liquid Propellant Rocket

Motor. Polytechnic Inst. of Brooklyn, New York, U.S. Air Force (con-

tract No. AF 49(638)-165), March 1962, 134 pp. Report No. AFOSK-2614.

Burstein, Samuel Z., Wallace Chinitz, and Harold Schechter. Nonlinear

Combustion Instability in Liquid-Propellant Rocket Motors (Final

Report). Mathematical Applications Group, Inc., White Plain, N.Y.,

Rept. No. MR-6903, June 1969. Jet Propulsion Lab. (contract

No. 951946), subcontracted from NASA (contract No. NAS 7-100).

II

120.

121.

122.

123.

124.

125.

126.

127.

128.

129.

130.

131.

Burstein, S. Z., S. Hammer, and V. D. Agosta. A Spray Combustion Model

With Droplet Breakup Including Gas Dynamic Coupling. Polytechnic

Inst. of Brooklyn, New York, U.S. Air Force (contract

No. AF 49(638)-165, Proj. No. 9751), June 1961. Report

No. AFOSR-TR-61-433.

Burton, Joe M. Additives for Nitric Acid. U.S. Pat. No. 2,994,190,

assigned to Phillips Petroleum Co., Aug. I, 1961.

Ignition Delay Reducing Agents for Hypergolic Rocket Fuels.

U.S. Pat. No. 2,993,33A, assigned to Phillips Petroleum Co., July 25,1961.

Busch, C. W. Generation of Flow Fields in Particle Fueled Combustion

Systems. Univ. of California at Berkeley, Report No. NASA-TN-I,

May 1965.

Busch, C. W., A. J. Laderman, and A. K. Oppenheim. Parametric Study of

the Generation of Pressure Waves by Particle-Fueled Combustion. Univ.

of California, Space Sciences Lab., Berkeley, Calif., 1965, 47 pp.

NASA (grant No. NsG-702/05-003-050).

. Pressure Wave Generation in Particle-Fueled Combustion Systems:

I. Parametric Study. AIAA J., v. &., No. 9, September 1966,

pp. 1638-1645. NASA (grant No. NsG-702/05-003-050).

Busch, C. W., A. S. Warnock, A. J. Laderman, and A. K. Oppenheim. Pres-

sure Wave Generation in Particle-Fueled Combustion Systems:

II. Influence of Particle Motion. AIAA J., v. 6, No. 2, February

1968, pp. 286-291. NASA (grant No. NsG-702/05-003-050).

Cain, E. F. C., F. C. Gunderloy, Jr., J. Sinar, and R. I. Wagner. Flow

Decay: Impaired Flow in Nitrogen Tetroxide Propulsion Systems Caused

by Corrosion Product Deposits. Rocketdyne, a Div. of North American

Rockwell Corp., Canoga Park, Calif., Rept. No. 7675, U.S. Air Force

Rocket Propulsion Lab., November 1968. Report No. AFRPL-TR-68-220.

Campbell, D. T., and W. D. Chadwick. Combustion Instability Analysis at

High Chamber Pressure (Final Report). Rocketdyne, a Div. of North

American Rockwell Corp., Canoga Park, Calif., Rept. No. R-7561, U.S.

Air Force (contract FO 4611-67-C-0036), August 1968, 174 pp. Report

No. AFRPL-TR-68-179.

Campbell, D. T., G. L. Cline, J. D. Cordill, R. L. Proffit, and

T. N. Sloat. Reactive Stream Separation Photography. Rocketdyne, a

Div. of North American Rockwell, Canoga Park, Calif., Rept. No. R-8110,

NASA-Jet Propulsion Lab. (contract No. NAS 7-720), Jan. I0, 1970.

Cantrell, R. H., and R. W. Hart. Interaction Between Sound and Flow in

Acoustic Cavities: Mass, Momentum, and Energy Considerations. J. of

the Acoustical Soc. of America, v. 36, No. 4, April 1964, pp. 697-706.

Cares, Janet Walkley. Determination of Formaldehyde by the Chromotropic

Acid Method in the Presence of Oxides of Nitrogen. American Indus-

trial Hygiene Assoc. J., v. 29, 1968, pp. 405-410.

Ill I/ .il II It 11 U i,I U !1 II 1I 11 11 il 11 1,1 K E g

12

132.

133.

134.

135.

136.

137.

i38.

139.

140.

141 .

142.

143.

Carrington, Tucker, and Norman Davidson.

ics: The Rate of Dissociation of N_O_.

v. 57, 1953, pp. 418-427.

Shock Waves in Chemical Kinet-

J. of Physical Chemistry,

Catton, I., D. E. Hill, and R. P. McRae. Study of Liquid Jet Penetra-

tion in a Hypersonic Stream. AIAA J., v. 6, No. II, November 1968,

pp. 2084-2089.

Caudill, Charles L., and Ronald L. Kirlin. Maraging Steel Propellant

Storability Test Tank. Martin Marietta Corp., Denver Div., Final

Rept. MCR-69-413, 9/10/68-8/8/69, September 1969, 48 pp. U.S. Air

Force (contract No. FO 4611-69-C-0029), Report No. AFRPL-TR-69-194.

Chang, E. T., and N. A Gokcen. Thermodynamic Properties of Gases in

Propellants and Oxidizers. I. Solubilities of He, Ne, Oe, Ar, and

NeO3 in Liquid NeO 4. J. of Phys. Chem., v. 70, No. 7, July 1966,

pp. 2394-2399.

Thermodynamic Properties of Hydrazine, Unsymmetrical Dimethyl-

hydrazine and Their Mixtures. Aerospace Corporation_ E1Segunda,

Calif., Rept. No. ATN-64(9228)-2, Jan. 8, 1964, 27 pp.

Chang, E. T., N. A. Gokcen, and T. M. Poston. Solubilities of Gases in

Simple and Complex Propellants. J. of Spacecraft and Rockets, v. 6,

No. I0, October 1969, pp. 1177-1180.

. Thermodynamic Propc_rties of Gases in Propellants. II. Solubil-

ities of Helium, Nitrogen, and Argon Gas in Hydrazine, Methy!hydrazine,

and Unsymmetrical Dimethylhydrazine. J. of Phys. Chem., v. 72, No. 2,

February 1968, pp. 638-642.

Cherepanov, G. P. Theory of Detonation in Heterogeneous Systems. (In

Russian.) Zh. Prikl. Mekhan. i Tekhn. Fiz. (J. Applied Mechanics and

Tech. Physics), No. 4, 1965, pp.-163-164.

Chilenski, J. j., and D. H. Lee. An Experimental Investigation of the

Performance of the Nitrogen Tetroxide-Hydrazine System in the Oxidizer-

Rich and Fuel-Rich Regions. Jet Propulsion Lab., California Inst. of

Technology, Tech. Rept. No. TR-32-212, Mar. 12, 1962.

Chinitz, W., and V. D. Agosta. Combustion Instability: Shock Wave

Propagation in a Liquid Propellant Rocket Motor. Polytechnic Inst. of

Brooklyn, New York, Rept. No. PRL-62-13, AFOSR (contract

No. AF 49(638)-165), June 1962, 94 pp.

Shock-Wave Propagation in Liquid Propellant Rocket Engines.

Pyrodynamics, v. I, October 1964, pp. 299-317.

Choudhury, A. P. Roy, G. G. Lamb, and W. F. Stevens. A New Technique

for Drop-Size Distribution Determination. Trans. I.I.Ch.E., v. X,1957-58, 1959, pp. 21-24.

11 I/ _iJ ]l,i Ii U IJ 1,' 11 IJ u li 11 11 11 g g

13

144.

145.

146.

147.

i48.

149.

150.

151.

152.

153.

Choudhury, P. Roy, and P. C. Wilber. Application of Semenov's Criterion

to Spontaneous Ignitions of N204 and N@H_ in Homogeneous and Hetero-

geneous Phases. Paper No. WSCI-67-37, pres. at the 1967 Fall Meeting

of the Western States Section Combustion Inst., Seattle, Wash., 1967.

A Semi-Empirical Analysis of the Hypergolicity of Gas-Gas and

Gas-Liquid Reactions of N@I_-N204 Type Propellants. Proc. of Seventh

Internat. Symposium on Space Technology and Science, Tokyo, 1967,

pp. 95-100.

Chretlen, Andre, and Oscar Hoffer. Sur la preparation et sur le dosage

de queiques sels min_raux; chlorure et nitrate d'hydrazinium-s_l_niate,

azoture, et isocyanate de potassium (On the Preparation and Analysis

of Some Inorganic Salts: Chloride and Nitrate of Hydrazine, Selenate,

Nitride, and Isocyanate of Potassium.) Bulletin de la Societe Chimique

de France, Set. 5, _, p.l, 1939, pp. 1587-1599.

Christos, Theodore, Yael Miron, Harry James, and Henry Perlee. Combus-

tion Characteristics of Condensed-Phase Hydrazine-Type Fuels With

Nitrogen Tetroxide. J. cf Spacecraft and Rockets, v. 4, No. 9,

September 1967, pp. 1224-1229.

. Exploration Study of Hypergolic ]ignition Spike Phenomena.

BuMines, Pittsburgh, Pa., Phase II--First Quart. Rept. No. 3986,

Jan. 1-Mar. 31, 1966; 32 pp. NASA, Houston, Tex. (order

No. T-39882(G)).

Exploration Study ¢f Hypergolic Ignition Spike Phenomena.

BuMines, Pittsburgh, Pa., Phase II, Part II, July 1-Sept. 30, 1966;

14 pp. NASA, Houston, Tex. (order No. T-39882(G)).

Chu, Boa-Teh, and S. J. Yir_. Thermally Driven Non Linear Oscillation

in a Pipe With Travelling Shock Waves. Brown Univ., Providence, R.I.,

U.S. Air Force Office of Scientific Res. (contract No. AF 49(638)-646),April 1961, 32 pp.

Chu, C. K. A Kinetic-Theoretic Descriptlon of the Formulation of a

Shock Wave. Columbia Univ., New York, Rept. No. ii, U.S. Air Force

(contract No. AF 94(638)-1254), June 1964, 41 pp.

Chuan, R. L., J. G. Everton, M. A. Merrigan, and P. C. Wilber. Propel-

lant Reaction Characteristics in Space Environmental Test Facilities.

Cellesco (Cellestial Research Corp.), Air Force Rocket Propulsion Lab.

(contract No. AF 04(611)-8392), Air Force System Command, ReportNo. AFRDL-TR-65-19, Jan. 15, 1965.

Chuan, Raymond L., and Paul C. Wilber. Ignition of Hypergolic Propel-

lants in a Simulated Space Environment. J. of Spacecraft and Rockets,v. 4, No. 2, February 1967, pp. 282-284.

U U ]iJ i,i IJ U E E U U U U 11 11 U B L

14

154.

155.

156.

157.

158.

159.

160.

161.

162.

163.

Clairmont, A. R., Jr., I. Jaffe, and D. Price. The Detonation Behavior

of Ammonium Perchlorate as a Function of Charge Density and Diameter.

U.S. Naval Ordnance Lab., White Oak, Md., June 20, 1967, 43 pp.

Report No. NOL-TR-67-71.

Clark, Bruce J. Propellant Vaporization as a Criterion for Rocket

Engine Design: Experimental Effect of Combustor Length, Throat Diam-

eter, Injection Velocity and Pressure on Rocket Combustor Efficiency.

Report No. NASA-TN-D-258, April 1960, 27 pp.

Clayton, Richard M. Recent Experimental Results From a Study of Reso-

nant Combustion. CPIA Pub. No. 138, v. i (February 1967), paper

pres. at the ICRPG 3d Combustion Conf. at NASA, John F. Kennedy Space

Center, Cocoa Beach, Fla., Oct. 17-21, 1966, NASA (contract

No. NAS 7-100), February 1967.

Clyne, M. A. A. Reactions of the HNO Molecule. lOth Symposium (Inter-

national) on Combustion, at the Univ. of Cambridge, Cambridge, England,

Aug. 17-21, 1964. Pub. by the Combustion Inst., 1965, pp. 311-316.

Coates, R. L., and M. D..Horton. Design Considerations for Combustion

Stability. J. Spacecraft, v. 6, No. 3, March 1969, pp. 296-302.

Coates, R. L_, M. D. Horten, and N. W. Ryan. T-Burner Method of Deter-

mining the Acoustic Admittance of Burning Propellants. AIAA J., v. 2,

No. 6, June 1964, pp. 1119-1122.

Cole, Leland G. Evaluaticn of the Performance Characteristics of the

N20_-NeH4 System. Jet Propulsion Lab., California Inst. of Technol-

ogy, Pasadena, Calif., Progress Rept. No. 9-48, Dept. of the Army,

Ordnance Corps (contract: No. DA-04-495-ORD 18), ORDC!T Project,

Nov. 15, 1950.

The Nitrogen Oxides as Rocket Fuel Oxidants Including the Theo-

retical Performances of Propellant Systems Employing Nitrogen Tetrox-

ide. Jet Propulsion Lab. Progress Rept. No. 9-23, California Inst. of

Technology, Pasadena, Calif.; Basic Res. on Rocket Propellants (con-

tract No. W-04-200-ORD-1482; Project No. TU2-1), Oct. 18, 1948.

Combs, L. P., W. D. Chadwick, D. T. Campbell. Liquid Rocket Performance

Computer Model With Distributed Energy Release. Rocketdyne, North

American Rockwell Corp., Interim Final Rept. No. 8298; NASA

(NAS 7-746), Jet Propulsion Lab., Pasadena, Calif., Sept. ii, 1970,

58 pp.

Combs, L. P., J. A. Murphy, E. E. Lockwood, F. W. Hoehn, and M.

Alexander. Combustion Stability Rating Techniques. Res. Dept. of

Rocketdyne, a Div. of North American Aviation, Inc., Canoga Park,

Calif., 2nd Quart. Progress Rept. No. R-6355-2 for period ending

Dec. 30, 1965; Air Force Rocket Propulsion Lab., Res. and Tech. Div.,

Edwards AFB (contract No. AF 04(611)-10811), January 1966.

]lJ ILl _]lJ IJ ]] U ],,[ L[ L[ 1,[ ],[ I/ L[ 1[ ].[ u u K E Z:

15

164.

165.

166.

167.

168.

169.

170.

171.

172.

173.

174.

Conn, T. E., J. N. Hester, and R. S. Valentino.

Upon Rocket Injector/Chamber Compatibility.

No. 12, December 1967, pp. 1581-1585.

Environmental Effects

J. Spacecraft, v. 4,

Coon, E. D. Some Observations on the Dissociation of NeO 4. Proc. of

North Dakota Acad. of Science, v. XVIII, 1964, pp. 108-111.

Cooper, James P., Glen W. Howell, L. N. Mortenson, and D. Kirschner.

Problems Encountered During Installation and Operation of a Storable

Propellant Facility for Testing of Titan II Components and Systems.

Wyle Laboratories, E1Segundo, Calif., Tech. Note 10235, Mar. 7, 1961,

66 pp. U.S. Air Force Ballistic Missile Div., Air Res. and Devel.

Command (contract No. AF 04(647)-398). Report No. AFBMD-TN-61-32.

Corbeau, Jean, and Claude Diot. Etude th_orique de la combustion de

gouttes d'ergols dans une chambre de combustion de propulseur-fusSe

(Theoretical Study of Propellant Droplet Combustion in a Rocket Motor).

IXth Internat. Astronautical Congress, Amsterdam 1958 Proceedings. ii.1958, pp. 526-556,

Corbett, A., T. Seamans, B. Dawson, and C. Cheetham. Hypergolic Igni-

tion at Reduced Pressures. Thiokol Chemical Corporation, Reaction

Motors Div., Denville, N.J., December 1964, 74 pp. Report

No. AFRPL-TR-64-175, Air Force Rocket Propulsion Lab., Edwards, Calif.

(contract No. AF 04(611)-9946).

Corbett, A. D., B. E. Dawson, T. F. Semnans, and M. M. Vanpee. Hyper-

golic Ignition at Reduced Pressures. Reaction Motors Div., Thiokol

Corp., Report No. AFRPL-TR-(EMD-5801-E, Part II), November 1965.

Corcoran, Jane M., Howard W. Kruse, Sol Skolnik, and Eugene Lieber.

Thermal Analysis of the System Hydrazine Nitrate-Water-Hydrazine.

U.S. Naval Ordnance Test Station, Inyokern, China Lake, Calif.,

Report Nos. NOTS-824, NAVORD-2087, Jan. 26, 1954, 14 pp.

Corcoran, William H., H. H. Reamer, and B. H. Sage. Volumetric and

Phase Behavior of the Nitric Acid-Nitrogen Dioxide System. Jet Pro-

pulsion Lab., California Inst. of Technology, Pasadena, Calif.,

Progress Rept. No. 20-173, Aug. i0, 1953, 24 pp. Dept. of the Army,

Ordnance Corps (contract No. DA-04-495-ORD-18), ORDCIT Project.

Cordes, Herman F. The Thermal Decomposition of I,I Dimethylhydrazine.

J. Phys. Chem., v. 65, September 1961, pp. 1473-1477.

Cordes, H. F., N. R. Fetter, and J. A. Happe. The Thermal Decomposition

of Liquid Nitric Acid. J. of the American Chem. Soc., v. 80, 1958,pp. 4802-4808.

Courtney-Pratt, J. S., and G. T. Rogers. Initiation of Explosion by

Light and by Flying Fragments. Nature, v. 175, No. 4458, Apr. 9, 1955,pp. 632-633.

Ii Ii 11 II Li U U li IJ IL 11 II 1t II £

16

175.

176.

177.

178.

179.

180.

181.

182.

183.

184.

185.

Crabb, James P. Experimental Precombustion Chamber/Injector Assembly

Development and Design Verification Tests. NASA-MSC, Houston, Tex.,

Internal Note No. MSC-IN-64-EP-II, Apr. 12, 1965.

Cramer, Frank B. Liquid Rocket Combustion Processes. Multi-Tech, Inc.,

Progress Rept. No. 4244-2; Jet Propulsion Lab., California Inst. of

Technology (contract No. 950926), subcontract under NASA (contract

NAS 7-100).

Cramer, Frank B., and William T. Webber. Liquid Rocket Combustion Pro-

cesses. Multi-Tech, Inc., Progress Rept. No. R-4244-3, PR-2; Jet Pro-

pulsion Lab., California Inst. of Technology (contract No. 950926),

subcontract under NASA (contract NAS 7-100), 1965.

Liquid Rocket Combustion Processes. Task I. Initiation of

Literature Survey. Multi-Tech, Inc., Progress Rept. No. 4244-1; Jet

Propulsion Lab., California Inst. of Technology (contract No. 950926),

subcontract under NASA (contract NAS 7-i00), 1964.

Cramer, Frank B., William T. Webber, and Robert B. Lawhead. Research on

the Basic Fluid Dynamic Phenomena Related to Rocket Combustion Insta-

bility. Rocketdyne, North American Aviation, Inc., Rept.

No. WADC-TN-57-426, June 1958. U.S. Air Force, Wright Air Development

Center (WADC) (contract No. AF-33(616)-3556).

Crocco, Luigi, Jerry Grey_ and David T. Harrje. On the Importance of

the Sensitive Time Lag in Longitudinal High-Frequency Rocket Combus-

tion Instability. Jet Propulsion, v. 28, No. 12, December 1958,

pp. 841-843.

Theory of Liquid Propellant Rocket Combustion Instability and

Its Experimental Verification. A.R.S.J., v. 30, 1960, pp. 159-168.

Curtius, Theodor, and Rudolf Jay. Diazo-und Azoverbindungen der

Fettreihe. IV. Abhandlung Ueber das Hydrazin (Diazo and Azo Combi-

nations of the Aliphatic Series. IV. Treatise on Hydrazine). J.

prakt, chemic, v. 147, 1889, p. 27.

Curzon, F. L. The Growth of Corrugations on Accelerated Fluid Sheets.

Canadian J. of Phys., v. 43, December 1965, pp. 2200-2211.

Cuy, E. J., and W. C. Bray. The Oxidation of Hydrazine. II. The

Effect of Oxygen on the Decomposition of Hydrazine. The Reactions

With Ferricyanide in Alkaline Solution, and Dichromate in Acid Solu-

tion. J. American Chem. Sot., v. 46, 1924, pp. 1786-1795.

Dabora, E. K., K. W. Ragland, A. A. Ranger, and J. A. Nicholls. Two

Phase Detonations and Drop Shattering Studies. The Univ. of Michigan,

Ann Arbor, Mich., Rept. No. UM-06324-3-T; Report No. NASA-CR-72225

(contract No. NASr 54(07)), April 1969.

if If .if lJ It It U lI 11 U U H il 11 It U if K £ K

17

186.

187.

188.

189.

190.

191.

192.

193.

194.

195.

196.

Danilowicz, Ronald L. Computer Code for Calculating Temperature Pro-

files in a Propellant Tank. NASA, Lewis Reg. Center, Cleveland, Ohio,

Report No. NASA-TM X-1556, April 1968.

Daskin, Walter. Evaporation From Sprays. Purdue Univ., Engineering

Experiment Station, Reg. Set. 127-135, Res. Bull. No. 128, 1955,

pp. 329-341.

Dawson, B. E., A. F. Lum, and R. R. Schreib. Investigation of Advanced

High Energy Space Propellant System. Thiokol Chemical Corp., Rept.

No. RMD-5507-F, NASA, June-November 1962.

Dean, D. S., and K. Bridgewater. Applications of Condenser Timers

to a Thrust Integrator and an Ignition Delay Timer. Royal Aircraft

Establishment, Farnborough, HANTS Rocket Propulsion Dept., Westcott,

Rept. No. RPD-23, November 1949.

Decugler, Robert P. An Experimental Investigation of Chemical Reaction

Between Propellant Tank Material and Rocket Fuels or Oxidizers When

Impacte_ by Small High Velocity Projectiles. Report No. NASA-TN-D-1882,

August 1963.

Dee, L. A., T. W. Owens, A. K. Webb, and J. T. Nakemura. The Catalytic

Decomposition of Hydrazine on Gold, Nickel and a Gold/Nickel Brazing

Alloy. Air Force Rocket Propulsion Lab., Air Force Systems Command,

Edwards, Calif., Report No. AFRPL-TR-69-77, April 1969.

Dee, L. A., and A. K. Webh. Gas Chromatographic Separation of Hydrazine

Mixtures and Water Using a Stationary Phase That Is Chemically Similar

to Hydrazine. Analytical Chem., v. 39, No. I0, August 1967,

pp. 1165-1167.

Delmonte, Julian. A Semiconductor Combustion Pressure Transducer for

Rocket-Motor Instability Studies. ISA Trans., v. 6, No. I, January

1967, pp. 9-14.

Denisov, Yu. N., and Ya. K. Troshin. On the Mechanism of Detonative

Combustion. 8th Symp. (International) on Combustion, Paper No. 62,

at the California Inst. of Technology, Pasadena, Calif., Aug. 28-

Sept. 3, 1960, pp. 600-610. Pub. by Williams and Wilkins Company,

1962.

De Vogelaere, R., and M. Boudart. Contribution to the Theory of Fast

Reaction Rates. Princeton Univ., James Forrestal Res. Center, Tech.

Rept. No. 3, July 1953. U.S. Air Force, Air Reg. and Devel. Command

(contract No. AF 33(038)-23976).

Dewar, Michael J. S., and Brian Jennings. Rotation-Inverslon Barriers

in Hydrazines. J. of American Chem. Sot., v. 91, No. 13, June 18,

1969, pp. 3655-3656.

18

197. Dickerson, R., K. Tate, and N. Barsic. Correlation of Spray InjectorParameters With Rocket Engine Performance. Rocketdyne, North AmericanRockwell Corp., CanogaPark, Calif., U.S.A.F., ReportNo. AFRPL-TR-68-147,June 1968.

198. Dickerson, R.A. Like and Unlike Impinging Injection Element DropletSizes. J. Spacecraft, v. 6, No. ii, November1969, pp. 1306-1308.

199.

200.

Diesen, R. W. Mass Spectral Studies Behind Shock Waves. II. The Ther-mal Decomposition of Hydrazlne. DowChemical Company,ARPALab.,Midland, Mich. Rept. No. AR-3S-63, Office of Naval Res. (contractNonr 3814-(00)), August 1963, 23 pp.

Dityakin, I. F., and V. I. Yagodkin. Effect of Periodic Oscillations ofVelocity and Density of a Mediumon Disintegration of Liquid Jets.Akad. Nauk. SSSR,Otdel Tekh. Nauk. No. 4, 1957. NASA(Tech. Transl.No. NASA-TT-F-63), April 1961.

201. Dobbins, ThomasO. Thermodynamicsof Rocket Propulsion and TheoreticalEvaluation of SomePrototype Propellant Combinations. Wright-Patterson Air Force Base, Wright Air Devel. Center, Rept.No. WADC-TR-59-757,December1959.

202. Dombroski, N., and P. C. Hooper. The Effect of Ambient Density on DropFormation in Sprays. Chem.Eng. Sci., v. 17, April 1962, pp. 291-305.

203. Donovan, Leo F., and Carroll A. Todd. Computer Program for CalculatingIsothermal, Turbulent Jet Mixing of TwoGases. ReportNo. NASA-TN-D-4378,March 1968.

204. Dresser, A L., A. W. Browne, and C. W. Mason. Anhydrous Hydrazine.VI. Hydrazine Trinitride Monohydrazinate, NeH_N3"N_H_. American Chem.Soc. J., v. 55, May 1933, pp. 1963-196}.

205. Drummond,L. J., and S. W. Hiscock. Shock-Initiated Exothermic Reac-tions. I. The Decomposition of Nitrous Oxide. Australian J. ofChem., v. 20, 1967, pp. 815-824.

206. Dubb, H. E., J. Fisher, B. C. Neale, J. Rosengard, and A. A-xworthy.Research and Engineering Data on Inhibited NsO4. Rocketdyne, NorthAmerican Rockwell Corp., CanogaPark, Calif., Rept. 7680 (Final Rept.),

January 1969, 114 pp. U.S. Air Force (contract No. AF 04(611)-10809).

Report No. AFRPL-TR-69-4.

207. Ducarme, J. Liquid Propellants for Rocket Engines. Compt. Rend. Congr.

Intern. Chim. Ind., 31", Liege L'Universite de Liege, 1958.

208. Dukes, E. K., and R. M. Wallace. Formation of Hydrazoic Acid From

Hydrazine in Nitric Acid Solutions. E. I. du Pont de Nemours and

Company, Savannah River Lab., Tech. Div., Aiken, S.C., Rept.

No. DP-728, U.S. Atomic Energy Commission (contract No. AT(07-2)-I),

September 1962, 17 pp.

111 II- jil U lIll U II U U II II 11 11 1I L L L

19

209.

210.

211.

212.

213.

214.

215.

216.

217.

218.

219.

Duncan, A. F., T. L. Kelly, and D. A. Moberg. A Study of Hypergolic

Bipropellant Mass Expulsion for Attitude Control of Spacecraft.

Marquardt Corp., Rept. No. ASD-TDR-62-1065, AF Flight Dynamics Lab.,

AFSC, Wright-Patterson AFB (contract No. AF 33(657)-7933), August1964.

Durig, J. R., S. F. Bush, and E. E. Mercer. Vibrational Spectrum of

Hydrazine-d 4 and a Raman Study of Hydrogen Bonding in Hydrazine. J.

of Chem. Phys., v. 44, No. ii, June I, 1966, pp. 4238-4247.

Dwiggins, R. D., and B. F. Larrick. Investigation of Mixtures of Hydra-

zine, Hydrazine Nitrate and Water. Part II. U.S. Naval Ordnance Lab.,

White Oak, Silver Spring, Md., Progress Rept. No. NAVORD-2563, cover-

ing the period from Apr. 1-June 30, 1952; Aug. 13, 1952.

Dykema, Owen W., and Stanley A. Greene. An Experimental Study of RP-I,

UDMH and NmH 4 Single Droplet Burning in Air and in Oxygen. Progr.

Astronaut. Rocketry, vt 2, pp. 299-324, U.S. Air Force (contract

No. AF 04(647)-171), 1960.

Eberstein, I. J., and I. Glassman. Consideration of Hydrazine Decompo-

sition. Progr. Astronaut. Rocketry, v. 2, 1960, pp. 351-366.

The Gas-Phase Decomposition of Hydrazine and Its Methyl Deriva-

tives. Tenth Symp. (International) on Combustion, at nhe Univ. of

Cambridge, Cambridge, England, Aug. 17-21, 1964, pp. 365-374. Pub.

by the Combustion Inst., U.S. Air Force, AFOSR (grant No. AF 62-90),

National Science Foundation (grant No. NSF-GF579), 1965.

Egly, Richard S., and Quentin R. Jeffries. Development of a Simple Sta-

bility Test for Monopropellants Utilizing a Detonating Cap and Heavy

Confinement. Commercial Solvents Corp., Res. and Devel. Div., Terre

Haute, Ind. (a paper pres. at the Western States meeting of the Com-

bustion Inst., 1965, WSCI-65-35), 1965.

Elgin, Joseph C., and Hugh S. Taylor. The Photosensitized and Photochem-

ical Decomposition Of Hydrazine. J. of the American Chem. Soc., v. 51,

July 5, 1929, pp. 2059-2082.

Ellis, George E. Literature Survey of the Kinetics of the H-O-N System.

Marquardt Corp., Memo. Rept. No. 20202, U.S. Air Force (contract

No. AF 33(657)-8491), November 1962.

Elverum, G. W., Jr., and Leland G. Cole. Some Physical-Chemical Studies

of the System Hydrazine-Hydrazine Nitrate and Water. Jet Propulsion

Lab., California Inst. of Technology, Pasadena, Calif., Memo.

No. 20-152, Dec. 22, 1957, 46 pp.

Some Physical-Chemical Studies of System Hydrazine-Hydrazine

Nitrate-Water. Jet Propulsion Lab., Memo. No. 20-79, California Inst.

of Technology, Pasadena, Calif., U.S. Army Ordnance Corps (contract

No. DA-04-495-ORD 18), Dec. 30, 1952, 14 pp.

20

220.

221.

222.

223.

224.

225.

226.

227.

228.

229.

230.

231.

Elverum, G. W., Jr., and J. S. Martinez. Results of Performance Calcu-

lations for NeO4-NeH_ Bipropellant System. Jet Propulsion Lab., Cali-

fornia Inst. of Technology, Pasadena, Calif., Memo. No. 20-174,

July 3, 1958. U.S. Army Ordnance Corps (contract No. DA-04-495-ORD-10).

Elverum, G. W., Jr., and T. F. Morey. Criteria for Optimum Mixture-

Ratio Distribution Using Several Types of Impinging-Stream Injection

Elements. Jet Propulsion Lab., California Inst. of Technology,

Pasadena, Calif., Memo. No. 30-5, NASA (contract No. NASw-6), Feb. 25,

1959, II pp.

Elverum, G. W., Jr., and P. StaudhanmQer. The Effect of Rapid Liquid

Phase Reactions on Injector Design and Combustion in Rocket Motors.

Jet Propulsion Lab., California Inst. of Technology, Progress Rept.

No. 30-4, NASA (contract No. NAS W-6), Aug. 25, 1959.

Emanuel, George. Kinetics of Complex Molecules in Aerodynamic Flows.

AZAA J., v. 7, No. 6, June 1969, pp. 1208-1212.

Endow, N., and R. A. Pasternak. Sorption of Oxygen at Very Low Pres-

sures by Molybdenum Films. J. of Vacuum Science and Technology, 1968,

pp. 340-342.

Erikson, T. A. Pure Shock Environment Testing of Condensed-Phase,

Unstable Materials. A.R.S.J., v. 30:, 1960, pp. 190-191.

Ermakova, S. K., V. M. Cherednichenko, and S. Ya. Pshezhetshii. Reac-

tion Kinetics and Explosion in the Nitrogen Dioxide-Butane System.

Russian J. of Phys. Chem., v. 35, No. I0, October 1961, pp. 1161-1164.

Erpenbeck, Jerome J. Stability of Idealized One Reaction Detonations.

The Physics of Fluids, v. 7, No. 5, May 1964, pp. 684-696.

Eschweiler, J. C., and H. W. Wallace. Liquid Rocket Engine Feed System

Dynamics by the Method of Characteristics. McDonnell Douglas Corp.,

Box 516, St. Louis, Mo. 63166.

Etheridge, F. G., and R. A. Boudreaux. Attitude-Control Rocket Exhaust

Plume Effects on Spacecraft Functional Surfaces. J. Spacecraft, v. 7,

No. i, January 1970, pp. 44-48.

Evans, David D., Howard B. Stanford, and Robert W. Riebling. The

Effect of Injector-Element Scale on the Mixing and Combustion of Nitro-

gen Tetroxide-Hydrazine Propellants. Jet Propulsion Lab., California

Inst. of Technology, Pasadena, Calif., Tech. Rept. No. 32-1178, NASA

(contract No. NAS 7-100), Nov. I, 1967.

Evans, E. A., and A. B. Walburn. Analysis of Two-Phase Impingement From

a Cryogen Vented in Orbit. J. of Spacecraft and Rockets, v. 6, No. i0,

October 1969, pp. 1189-1193.

21

232.

233.

234.

235.

236.

237.

238.

239.

240.

Evans, J. I., and A. M. Yuill. Initiation of Condensed Explosives by

Compression of the Surrounding Gas. Proc. of the Royal Soc. (London),

Ser. A, Mathematical and Phys. Sci., v. 246, July-August 1958,

pp. 176-180.

Exler, R. A. Apollo Engine Start Characteristics Test Results. Rocket-

dyne, North American Aviation, Inc., Rept. No. SER 4390-6011, NAA,

S & ID Div., June 8, 1964.

Eyster, E. H., and L. C. Smith. Studies of the ERL Type 12 Drop-Weight

Impact Machine at NOL (NOL-37-Re2C-19-1b). U.S. Naval Ordnance Lab.,

White Oak, Silver Spring, Md., Memo. No. 10,003, 1949.

Eyster, E. H., L. C. Smith, and S. R. Walton. The Sensitivity of High

Explosives to Pure Shocks (NOL-37-Re2G-19-1b). U.S. Naval Ordnance

Lab., White Oak, Silver Spring, Md., Memo. No. 10,336, July 14, 1949.

Falkenstein, G., and H. Burge. Attitude Control Engine Ignition Model.

Rocketdyne, North American Aviation, Inc., Internal Letter

No. UM-361-64-135, July 6, 1964.

Farber, E. A. A Mathematical Model for Defining Explosive Yield and

Mixing Probabilities. "The Challenge of Space," Proc. of the Third

Space Congress, Cocoa Beach, Fla. (Mar. 7-10, 1966), NASA, Tech. Paper

No. 346 (part of contract NAS 10-1255), March 1966.

Farber, E. A., and J. H. Beese. A Systematic Approach for the Analyti-

cal Analysis and Prediction of the Yield From Liquid Propellant Explo-

sions. "The Challenge of Space," Pro¢. of the Third Space Congress,

Cocoa Beach, Fla. (Mar. 7-10, 1966), NASA, Tech. Paper No. 347 (part

of contract NAS 10-1255), March 1966.

Farber, E. A., and J. S. Gilbert. Characteristics of Liquid Rocket Pro-

pellant Explosion Phenomena. No. 387. Part IV. Fireball Hypothesis

Describing the Reaction Front and Shock Wave Behavior in Liquid Pro-

pellant Explosions. Engineering Progress at the Univ. of Florida,

v. XXI, No. 8, August 1967. (Pub. monthly by the Florida Engineering

and Industrial Experiment Station, Coll. of Eng., Univ. of Florida.)

NASA (contract No. NAS 10-1255), 1967.

Farber, E. A., and R. L. San Martin. Characteristics of Liquid Rocket

Propellant Explosion Phenomena. No. 386. Part III. Studies and Analy-

sis of the Mixing Phenomena of Liquid Propellants Leading to a Yield-

Time Function Relationship. Engineering Progress at the Univ. of

Florida, v. XXI, No. 8, August 1967. (Published monthly by the

Florida Engineering and Industrial Experiment Station, Coll. of Eng.,

Univ. of Florida.) NASA (contract No. NAS 10-1255), 1967.

I! II II II II 1I lI It U II II II 11 II il 11 g E

22

241.

242.

243.

244.

245.

246.

247.

248.

249.

250.

251.

Farber, Erich A. Characteristics of Liquid Rocket Propellant Explosion

Phenomena. No. 415A. Part VI. Explosive Yield Estimates for Liquid

Propellant Rockets Based Upon a Mathematical Model. Engineering

Progress at the Univ. of Florida, v. XXII, No. 7, July 1968. (Pub-

lished monthly by the Florida Engineering and Industrial Experiment

Station, Coll. of Eng., Univ. of Florida.) NASA (contract

No. NAS 10-1255), 1967.

Characteristics of Liquid Rocket Propellant Explosion Phenomena.

No. 415B. Part VII. Interpretation of Explosive Yield Values

Obtained From Liquid Rocket Propellant Explosions. Engineering Prog-

ress at the Univ. of Florida, v. XXII, No. 7, July 1968. (Published

monthly by the Florida Engineering and Industrial Experiment Station,

Coll. of Eng., Univ. of Florida.) NASA (contract No. NAS 10-1255),

1967.

Farber, Milton, and Alfred J. Darnell. Spectroscopic Examination of the

NH_-HNO_ and NHs-NO e Diffusion Flames. J. of Chem. Phys., v. 22, 1954,

pp. 1261-1263.

Felberg, Robert S, and Jack R. Gould. Rocket Fuel and Fuel Additive.

U.S. Pat. 2,900,788, assigned to the Thiokol Chemical Corp., Aug. 25,1959.

Fendell, Francis E. Combustion in Initially Unmixed Reactants for One-

Step Reversible Chemical Kinetics. Astronautica Acta, v. 13, 1967,

pp. 183-i91.

Decompositional Burning of a Droplet in a Small Peclet Number

Flow. AiAA J., v. 6, No. I0, October 1968, pp. 1946-1953.

Finite-Rate Burning of a Monopropellant Droplet in a Stagnant

Atmosphere. Astronautica Acta, v. II, No. 6, 1965, pp. 418-421.

• Flame Structure in Initially Unmixed Reactants Under One-Step

_etics. Chem. Eng. Sci., v. 22, 1967, pp. 1829-1837.

Ignition and Extinction in Combustion of Initially Unmixed React-

ants. J. of Fluid Mechanics, v. 21, part 2, 1965, pp. 281-303.

Multiplicity of Burning Modes in Initially Unmixed Reactants

Under One-Step Kinetics. AIAA Paper No. 66-71, pres. at the 3d Aero-

space Sci. Meeting, New York, Jan. 24-26, 1966.

Ferri, A., P. A. Libby, and V. Zakkag. Theoretical and Experimental

Investigation of Supersonic Combustion. From the book '_igh Tempera-

tures in Aeronautics and Astronautics" (Proc. of Symp. held in Turin,

Italy). International Series of Monographs in Aeronautics and Astro-

nautics, Carlo Ferrari, ed., MacMillan, 1962, pp. 55-118.

23

252.

253.

254.

255.

256.

257.

258.

259.

260.

261.

262.

263.

Fletcher, Robert F. Liquid-Propellant Explosions. J. of Spacecraft andRockets, v. 5, No. I0, October 1968, pp. 1227-1229.

Fletcher, Robert F., Dal Gerneth, and Clark Goodman. Explosion of Pro-pellants. AIAA J., v. 4, No. 4, April 1966, pp. 755-757.

Fogler, Scott. The Influence of Reacting Gases on the Motion of Collaps-ing Cavities. Chem.Eng. Sci., v. 24, 1969, pp. 1043-1054.

Fortini, Anthony. Performance Investigation of a NonpumpingRocket-Ejector System for Altitude Simulation. Report No. NASA-TN-D-257,December1959.

Foster, H. H., and M. F. Heidmann. Spatial Characteristics of WaterSpray Formedby Two Impinging Jets at Several Jet Velocities inQuiescent Air. Report No. NASA-TN-D-301,July 1960.

Franklin, J. L., John T. Herron, Paul Bradt, and Vernon H. Dibeler.American Chem.Soc. J., v. 80, 1958, pp. 6188-6190.

Fraser, R. P. Liquid Atomisation. J. of the Royal Aeronautical Soc.,v. 65, November1961, pp. 749-755.

Freeman, J. P., and William D. Emmons. The Reaction of DinitrogenTetroxide With Acetylenes. American Chem.Soc. J., v. 79, Apr. 5,1957, pp. 1712-1716.

Friedman, Morton H. Shock TubeMeasurenmntof Explosive Sensitivity.Minnesota Mining and Manufacturing Company,St. Paul, Minn. (a paperpres. at the Western States meeting of the Combustion Inst., 1965,Paper No. WSCI-65-32), 1965, 17 pp. AdvancedRes. Proj. Agency andBureau of Naval Weapons(contract NOB.NOrd 18688and Now-64-0399-C),1965.

A Correlation of Impact Sensitivities by Meansof the Hot SpotModel. 9th Symp. (International) on Combustion (at Cornell Univ.,Ithaca, N.Y., Aug. 27-Sept. i, 1962). Pub. by theAcademic Press,1963, pp. 294-302.

Friedman, R., W. P. Barnes, Jr., and M. Markels, Jr. A Study of Explo-sions Induced by Contact of Hydrazine-Type Fuels With Nitrogen Tetrox-ide. (Task V) Atlantic Res. Corp., Alexandria, Va., 9th Quart.Progress Rept. (for the period Dec. i, 1961-Feb. 28, 1962), 14 pp.Aeronautical Systems Div., Wright-Patterson Air Force Base, Ohio(contract No. AF 33(616)-6918), March 1962.

A Study of Explosions Induced by Contact of Hydrazine-Type FuelsWith Nitrogen Tetroxlde. (Final Rept.) Atlantic Res. Corp., Alex-andria, Va, September 1962, 31 pp. Flight Accessories Lab., Aero-nautical Systems Div., Air Force Systems Com_nand,WPAFB,Ohio (con-tract No. AF 33(616)-6918), Report No. ASD-TDR-62-685.

U U U L

24

264.

265.

266.

267.

268.

269.

270.

271.

272.

273.

274.

275.

Friedman, Raymond. High-Temperature Durability of Molybdenum in Oxygen-

Deficient Combustion Gases. J. of the American Rocket Soc. (Jet Pro-

pulsion), v. 24, May-June 1954, p. 187.

Friedman, Robert, Raymond E. Gaugler, and Erwin A. Lezberg. Expansion

of Simulated Storable Propellants in a Supersonic Nozzle. AIAA J.,

v. 7, No. 6, June 1969, pp. 1115-1118.

Experimental Measurements of Expanding Storable-Propellant Prod-

ucts Simulated by Combustion of Gaseous Reactants. NASA, Lewis Res.

Center, Cleveland, Ohio, September 1969, 25 pp. ReportNo. NASA TN-D-540.

Frierson, Wallace B. A Protection Against Toxic Rocket Fuels.

American Industrial Hygiene Assoc. J., v. 29, September-October 1968,

pp. 456-460.

Fuhs, A. E. Spray Formation and Breakup, and Spray Combustion. Sund-

strand Turbo, a div. of Sunstrand Machine Tool Co., Air Force Office

of Sci. Res., U.S. Air Force (contract No. AF 18(603)-107); Feb. 5,

1958, 129 pp. Report No. AFOSR-TN-58-414.

Furno, Aldo L., Agnes C. Imhof, and Joseph M. Kuchta. Effect of Pres-

sure and Oxidant Concentration on Autoignition Temperatures of

Selected Combustibles in Various Oxygen and Nitrogen Tetroxide Atmos-

pheres. J. of Chem. and Eng. Data, v. 13, No. 2, April 1968,

pp. 243-249.

Furno, Aldo L., George H. Martindill, and Michael G. Zabetakis. Limits

of Flarmnability of Hydrazine-Hydrocarbon Vapor Mixtures. BuMines

Rept. of Inv. 6505, 1964, 7 pp. Westvaco-Chlor-Alkaii Div. of the

Food Machinery and Chem. Corp., Princeton, N.J.

Gerlach, C. Richard.

Excited Containers.

pp. 553-560.

Gayle, J. B., and J. W. Bransford. Size and Duration of Fireballs From

Propellant Explosions. NASA, George C. Marshall Space Flight Center,

Huntsville, Ala., Propulsion and Vehicle Eng. Lab., Report

No. NASA-TM-X-53314, Aug. 4, 1965.

Surface Disintegration of Liquid in Longitudinally

J. of Spacecraft, v. 5, No. 5, May 1968,

Gerneth, Dal C., and Clark Goodman. Chemical Explosions in Space.

Houston Res. Inst., Inc., Houston, Tex., Progress Rept. for the period

July 1-Oct. 15, 1964, NASA (contract bIAS 9-2640), Oct. 23, 1964.

Gerstein, Melvin. Correlation and Prediction of Flame Properties With

Special Reference to Liquid Hydrazine. A.R.S.J., v. 29, July 1959,

pp. 514-516.

Gilbert, M. The Hydrazine Flame. Combustion and Flame, v. 2, 1958,

pp. 137-148.

I/ I1 II IJ IJ tl l.i LI II 11 U rd kl 11 It U u K L l;

25

276.

277.

278.

279.

280.

281.

282.

283.

284.

285.

286.

287.

Kinetics of Hydrazine Decomposition in a Laminar Non-isothermal

Flow. Combustion and Flame, v. 2, 1958, pp. 149-156.

Glaskova, A. P. Effet des catalyseurs sur la deflagration du nitrate

d'ammonium et de ses melanges (Effect of Catalysts on the Deflagration

of Ammonium Nitrate and Its Mixtures). Explosifs, v. 20, No. I, 1967,

pp. 5-13.

Glassman, Irvin. Combustion Processes in Liquid Propellant Rocket

Motors. Princeton Univ., Dept. of Aeronautical Eng., New Jersey,

final rept. for period Sept. I, 1955-Aug. 31, 1960; Dec. 20, 1961,

5 pp. U.S. Air Force (contract No. AF 18(600)-1527).

Combustion Processes in Liquid Propellant Rocket Motors.

Princeton Univ., New Jersey, final rept. for period Sept. i, 1965-

Aug. 31, 1968; Mar. 15, 1969. U.S. Air Force (contract

No. AF 49(638)-1268). Report No. AFOSR 69-078TR.

Glatts, G. S. Stability Tests of Monopropellants Exposed to Flames and

Rifle Fire. Jet Propulsion Lab., California Inst. of Technology,

Pasadena, Calif., Tech. kept. No. 32-172, February 1962, ii pp.

Glenn, L. A. Recondensation From a Particle-Vapor Source Flow Into

Vacuum. AIAA J., v. 7, No. 4, April 1969, pp. 593-597.

Stationary Radial Source Flow of Liquid Particles into Vacuum.

AIAA J., v. 7, No. 3, March 1969, pp. 443-450.

Glowa, W., R. A. Hagstrom, A. W. Jache. Gas Chromatographic Methods for

Liquid propellant Analys:.s. O_in Mathieson Corp., Quart. Progress

Rept. No. 10381-1, Mar. 15, 1965. Report No. AFRPL-TR-65-69, USAFRPL,

Edwards AFB, Calif. (contract No. AF 04(611)-10381).

Goodman, Clark. Blast and Fireball Comparison of Cryogenic and Hyper-

golic Propellants. Final Report. Houston Res. Inst., Inc., Houston,

Tex., NASA (contract No. NAS 9-3506), Aug. 28, 1964, 161 pp.

Gordon, Alvin S. The Reaction Between Hydrazine and Hydrogen Peroxide

in the Liquid Phase. Third Symp. on Combustion and Flame and Explo-

sion Phenomena, Paper No. 61, held at the Univ. of Wisconsin, Madison,

Wis., Sept. 7-11, 1948, pp. 493-497. Pub. by the Williams and Wilkins

Company, Baltimore, Md., 1949.

Gordon, Sanford, and Frank J. Zeleznik. A General IBM 704 or 7090 Com-

puter Program for Computation of Chemical Equilibrium Compositions,

Rocket Performance, and Chapman-Jouguet Detonations, Supplement l-

Assigned Area-Ratlo Performance. Report No. NASA-TN-D-1737, October 1963.

Gore, Marvin R., and John J. Carroll. Dynamics of a Variable Thrust,

Pump Fed, Bipropellant, Liquid Rocket Engine System. Jet Propulsion,

v. 27, No. I, January 1957, pp. 35-43.

I/ li liJ II II i,i l.I LI U U I,I M 11 U 11 U g E if

26

288.

289.

290.

291.

292.

293.

294.

295.

296.

297.

298.

Goulden, J. D. S., and D. J. Millen. Vibrational Spectra of ionic Forms

of Oxides and Oxy-acids of Nitrogen. Part VI. Raman-Spectral Evi-

dence of the Ionisation of Dinitrogen Tetroxide in Nitric Acid. The

Nitrosonium Ion, NO+ , and the Nitrosonium-Nitrogen Dioxide Ion, N_Oa +

J. of the Chem. Soc. (London), 1950, pp. 2620-2627.

Gowenlock, B. G. The Inhibition of Gaseous Free Radical Chain Reactions.

Progress in Reaction Kinetics, v. 3, Ch. 4, G. Porter, editor,

pp. 173-179; Pergamon Press, 1965.

Gray, P. Equilibrium Between a Condensed Phase and a Reactive Vapour:

The Heat Capacity of a Saturated, Dissociating Vapour and the Form of

the Vapour Pressure Curve. Proc. of the Royal Soc., No. 1319, v. 264,

December 1961, pp. 516-539.

Gray, P., and M. J. Harper. The Thermal Theory of Induction Periods and

Ignition Delays. Seventh Symp. (International) on Combustion, Paper

No. 61, at London and Oxford, Aug. 28-Sept. $, 1958. Pub. by the Com-

bustion Inst., 1959, pp. 425-430.

Gray, P., and J. C. Lee. The Combustion of Gaseous H}drazine. Trans.

Faraday Soc., v. 50, January 1954, pp. 719-728.

Explosive Decomposition and Combustion of Hydrazine. Fifth Symp.

(International) on Combustion, Combustion in Engines and Combustion

Kinetics, Paper No. 77, pres. at the Univ. of Pittsburgh, Pittsburgh,

Pa., Aug. 30-Sept. 3, 1954, pp. 692-700. Pub. by Reinhold Publishing

Corp., New York, 1955.

Recent Studies of the Oxidation and Decomposition Flames of

Hydrazine. 7th Symp. (International) on Combustion, Paper No. ii,

at London and Oxford, Aug. 28-Sept. 3, 1958, pp. 61-67. Pub. by the

Combustion Inst., 1959.

Gray, P., J. C. Lee, H. A. Leach, and D. C. Taylor. The Propagation and

Stability of the Decomposition Flame of Hydrazine. 6th Symp. (Inter-

national) on Combustion, Paper No. 31, at Yale Univ., New Haven, Conn.,

Aug. 19-24, 1956, pp. 255-263. Pub. by Reinhold Publishing Co., 1957.

Gray, P., J. C. Lee, and M. Spencer. Combustion, Flame and Explosion of

Hydrazine and Ammonia. 1--The Spontaneous Ignition of Pure Gaseous

Hydrazine. Combustion and Flame, v. 7, December 1963, pp. 315-321.

Gray, P., and M. Spencer. Combustion of Unsymmetrical Dimethylhydrazine:

Spontaneous Ignition in Decomposition and Oxidation. Combustion and

Flame, v. 6, December 1962, pp. 337-345.

Studies of the Combustion of Dimethyl Hydrazine and Related Com-

pounds. 9th Symp. (International) on Combustion, at Cornell Univ.,

Ithaca, N.Y., Aug. 27-Sept. i, 1962, pp. 148-157. Pub. by the Com-bustion Inst., 1963.

lff lff lff lff 11 II IZ U U ',a, U 11 11 ii 1[ g E L

27

299.

300.

301 •

302.

303.

304.

305.

306.

307.

308.

309.

310.

Thermal Explosions in the Oxidation of Hydrazine by Nitric Oxide

and Nitrous Oxide. Trans. of the Faraday Soc., v. 59, No. 484, April

1963, pp. 879-885.

Gray, Peter, and T. C. Waddington. Decomposition, Explosion _and Combus-

tion of Solid Ammonium Azide. Res. Correspondence, Supp. to Res.

(London), v. 8, No. II, 1955, pp. 556-557.

Gray, Peter, and A. D. Yoffe. The Reactivity and Structure of Nitrogen

Dioxide. Chem. Reviews, v. 55, 1955, pp. 1069-1154.

Greer, H., and D. J. Griep.

Reaction Jets in a Vacuum.

pp. 983-990.

Dynamic Performance of Low-Thrust, Cold-Gas

J. Spacecraft, v. 4, No. 8, August 1967,

Gregory, C. A., Jr., and H. F. Calcote. Combustion Studies of Droplet-

Vapor Systems. 4th Symp. (International) on Combustion, Paper No. 104,

at Massachusetts Inst. of Technology, Cambridge, Mass., Sept. 1-5,

1952, pp. 830-837. Pub. by Williams and Wilkins Company, 1953.

Greig, J. D., and P. G. Hall. Thermal Oxidation of Nitric Oxide at Low

Concentrations. Trans. of the Faraday Soc., v. 63, January-March 1967,pp. 655-661.

Grier, Norman T. Back Flow From Jet Plumes in Vacuum. NASA, Lewis Res.

Center, Cleveland, Ohio, January 1969. Report No. NASA-TN-D-4978.

Griffin, Donald N., and Edwin M. Clark. Effect of Low-Temperature and

Subatmospheric Chamber Pressure on Ignition Delay of RFNA-Aniline--

Furfuryl Alcohol Propellant Systems. Jet Propulsion Lab., California

Inst. of Technology, Pasadena, Calif., Progress Rept. No. 1-78,

Sept. 25, 1951, 19 pp. Air Materiel Co-_and (contract

No. W535-AC-20260).

Griffin, Donald N., and Donald R. Feller. Method for Initiating the

Combustion of Hydrazine. U.S. Pat. 3,021,667, assigned to Olin

Mathieson Chem. Corp., Feb. 20, 1962.

Groeneweg, John F. Measured Effects of Gaseous Flow System Dynamics on

Acoustic-Mode Combustion Instability. Report No. NASA TN-D-5080,

Lewis Res. Center, Cleveland, Ohio, March 1969.

Grundeis, L. Final Summary Report on the Development of Monopropellant

Test Equipment. Sundstrand Turbo, Rept. No. S/TD-1719, July 1959.

Wright-Patterson AFB, Wright Air Devel. Center (contract

No. AF 33(616)-5851).

Guhse, Richard D. An Experimental Investigation of Thrust Vector Con-

trol by Secondary Injection. Purdue Univ., Report No. NASA-CR-297,September 1965, 113 pp.

28

311.

312.

313.

314.

315.

316.

317.

318.

319.

320.

321.

322.

Gunder, D. F., and D. R. Friant. Stability of Flow in a Rocket Motor.American Soc. of Mech. Eng.; Trans., v. 72, 1950, pp. 327-333.

Gurnitz, R. N., T. R. Mills, J. D. Cordill, and G. L. Falkenstein. AComparisonof Nitrogen Tetroxide/Monomethylhydrazine and HydrogenPeroxide/Monomethylhydrazine Ignition Pressure Spiking Characteristics.Vol. II. A Study of Ignition Pressure Spiking in Attitude ControlEngines. Rocketdyne, CanogaPark, Calif., Rept. No. R-7060-2, May1967. NASA(contract No. NAS9-6134).

Gurnitz, R. N., T. R. Mills, and G. L. Falkenstein. Evaluation of theUse of Catalytic Surfaces To Eliminate Ignition Pressure Spiking.Vol. I. From a Study of Ignition Pressure Spiking in Attitude ControlEngines. Rocketdyne, CanogaPark, Calif., Rept. No. R-7060-I, May1967. NASA(contract No. NAS9-6134).

Hagstrom, R. A. Gas Chromatographic Methods for Liquid Propellant Anal-ysis. Olin Mathieson Chem.Corp., Quart. Progress Rept. No. 10381-2,June 15, 1965. U.S. Air Force Rocket Propulsion Lab. (contractNo. AF 04(611)-10381). Report No. AFRPL-TR-65-137.

Hall, A. R. Flame Speeds in Hydrazine Vapour at Low Pressures. RocketPropulsion Dept., Royal Aircraft Estab., Farnborough, Hants, GreatBritain, Rept. No. RPD-TN-129,September 1955, 12 pp.

Hydrazine Decomposition Flames at Sub-Atmospheric Pressures.Trans. Faraday Soc., v. 52, 1956, pp. 1520-1525.

Hall, A. R., and R. C. Murray. Further Experiments on Behavior of Self-Igniting Bi-Propellan _ at Sub-Atmospheric Pressures. Rocket Propul-sion Dept., Royal Aircraft Estab., Farnborough, Hants, Great Britain,Tech. Note No. Chem. 1056, R.P.D. No. 6, October 1948.

Hall, A. R., and H. G. Wolfhard. Hydrazine Decomposition Flames at Sub-atmospheric Pressures. Trans. Faraday Soc., v. 52, 1956,pp. 1520-1525.

Halliday, Kenneth C., Jr. Ignition System for Rocket Motors. U.S.Pat. 2,949,006, assigned to the U.S. of America as represented by theSecretary of the Army, Aug. 16, 1960.

Hamilton, Bob R. Operation of Reaction Motors. U.S. Pat. 2,994,191,assigned to Phillips Petroleum Company,a corporation of Delaware,Aug. i, 1961.

Hammer,Sanford S., and Vito D. Agosta. Longitudinal WavePropagationin Liquid Propellant Rocket Motors. ALEAJ., v. 2, No. II, November1964, pp. 2042-2044.

Hamrick, Joseph T., and Leslie C. Rose. Method of Igniting Rocket Fuels.U.S. Pat 3,101,589, assigned to ThompsonRamoWooldridge, Inc., Cleve-land, Ohio, Aug. 27, 1963.

29

323.

324.

325.

326.

327.

328.

329.

330.

331.

332.

333.

334.

Hanks, Brantley R., and David G. Stephens.

Resonant Frequencies in Propellant Lines.

October 1969, pp, 1202-1204.

Helium Injection To Reduce

J. Spacecraft, v. 6, No. i0,

Hanratty, T. J., J. N. Pattison, J. W. Clegg, and A. W. Ler_non, Jr.

Thermal Decomposition of Hydrazine Vapor in Silica Vessel. Ind. and

Eng. Chem., v. 43, No. I, May 1951, pp. 1113-1116.

Hanson, A0 R., and E. G. Domich. The Effect of Liquid Viscosity on the

Break-Up of Droplets by Air Blasts--A Shock Tube Study. Univ. of

Minnesota, U.S. Navy Bureau of Aeronautics, June 1956.

Harris, Frank E., and Leonard K. Nash. Determination of Traces of Water

Vapor in Gases. Analytical Chem., v. 23, No. 5, May 1951, pp. 736-739.

Harrje, D. T., and F. H. Reardon. Combustion Instability in Liquid

Propellant Rocket Motors, Thirty Second Quarterly Progress Report.

Princeton Univ., Aeronautical Eng. Dept., Rept. No. AER-216-ff,

June 13, 1960.

Combustion Instability in Liquid Propellant Rocket Motors,

Thirty Third Quarterly Progress Report. Princeton Univ., Aeronauti-

cal Eng. Dept., Rept. No. AER-216-gg, Dept. of the Navy (NOas-60-

6078-C), Nov. i, 1960.

Cor_ustion Instability in Liquid Propellant Rocket Motors,

Thirty Fourth Quarterly Progress Report. Princeton Univ., Aeronauti-

cal Eng. Dept., Rept. No. AER-216-hh, Dept. of the Navy (NOas-60-

6078-C), Nov. 15, 1960.

Combustion Instability in Liquid Propellant Rocket Motors.

Princeton Univ., Aeronautical Eng. Dept., Rept. No. AER-216-ii, Dept.

of the Navy (NOw-61-0686 d), June i, 1961.

Harrje, David T., and William A,. Sirignano. Nonlinear Aspects of Com-

bustion Instability in Liquid Propellant Rocket Motors. Princeton

Univ., Dept. of Aerospace and Mech. Sol., Tech. Rept. No. TR-553-d,

NASA (NASr-217), June i, 1964.

Nonlinear Aspects of Combustion Instability in Liquid Propellant

Rocket Motors. Princeton Univ., Dept. of Aerospace and Mech. Sci.,

Tech. Rept. No. TR-553-e, NASA, June l, 1965.

Hauptman, M. H., and H. Fine. Technique To Evaluate Surface Contamina-

tion Due to Rocket Exhaust Impingement. J. Spacecraft, v. 4, No. 8,

July 1967, pp.. 959-960.

Hay, J. E., and R. W. Watson. Mechanisms Relevant to the Initiation of

Low-Velocity Detonations. Annals of the New York Acad. of Sci.,

v. 152, art. I, Oct. 28, 1968, pp. 621-635. Bureau of Weapons, U.S.

Dept. of the Navy (Project 19-66-8027 WEPS).

3O

335.

336.

337.

338.

339.

340.

341.

342.

343.

344.

345.

346.

Heath, G. A., and G. R. Ramsden. The Continuous Measurement of Local

Mixture Ratio in Rocket Engines by a Mass Spectrometric Technique.

of the British Interplanetary Soc., v. 20, part i, February 1965,

pp. 1-6.

J°

Heidmann, Marcus F. Experimental Effect of Gas Flow Transients on the

Heat Release of Burning Liquid Drops in a Rocket Combustor. Report

No. NASA-TN-D-1576, LewlsRes. Center, Cleveland, Ohio, March 1963, 19 pp.

. Oxygen-Jet Behavior During Combustion Instability in a Two-

Dimensional Combustor. Report Ng. NASA-TN-D-2725, Lewis Res. Center,

Cleveland, Ohio, March 1965, 12 pp.

Heidmann, Marcus F., and H. H. Foster. Effect of Impingement Angle on

Drop Size Distribution and Spray Pattern of Two Impinging Water Jets.

Report No. NASA-TN-D-872, Lewis Res. Center, Cleveland, Ohio, July 1961.

Heidmann, Marcus F., and John F. Groeneweg. Dynamic Response of Liquid

Jet Breakup. AIAA J., v. 6, No. I0, October 1968, pp. 2033-2035.

Held, Manfred. Ballistics of Projectile Splinters (Splitterballistic).

In Three Parts. Explosivstoffe; part i: v. 15, No. 12, December 1967,

pp. 265-274; part 2: v. 16, No, 3, March 1968, pp. 49-55; part 3:

v. 16, No. 4, April 1968, pp. 73-78.

Initiierung yon Sprengstoffen, ein Vielschichtiges Problem der

Detonationsphysik (Initiation of Explosives. A Multi-Facet Problem of

Detonation Physics). Explosivstoffe, Zeitschrift f_r das Spreng-,

Schiep-, Z_nd-, Brand- und Gasschutzwesen, v. 16, No. 5, May 1968,

pp. 98-113.

Henderson, Ulysses V., Jr., and Welby G. Courtney. Process of Preparing

Hydrazinium Azide. U.S. Pat. 3,155,456, assigned to Texaco Experiment

Inc., Richmond, Va., Nov. 3, 1964.

Hennings, Glen, and Gerald Morrell. Low Temperature Chemical Starting

of a 200-Pound-Thrust JP-4-Nitrlc A_¢id Rocket Engine Using a Three-

Fluid Propellant Valve. Report No. NACA-RM-E55E04, June 30, 1955.

Herget, W. F., R. L. Proffit, and J. E. Witherspoon. Rocket Combustion

Stability Monitoring by Temporal Radiometry. J. Spacecraft, v. 6,

No. ii, November 1969, pp. 1336-1338.

Herickes, Joseph A., Glenn H. Damon, and Michael G. gabetakis. Determi-

nation of the Safety Characteristics of Unsymmetrical Dimethylhydra-

zine. BuMines Summary Rept. No. 3565, Jan. 15, 1957, 9 pp. Westvaco

Chlor-Alkali Div., Food Machinery and Chem. Corp. (contract

No. 14-09-050-1240).

Determining the Safety Characteristlcs of Unsymmetrical Dimethyl-

hydrazine. BuMines Rept. of Inv. 5635, 1960.

il IS ILl i,i U U U il U tl ti il 11 - u g £ [

31

347.

348.

349.

350.

351.

352.

353.

354.

355.

356.

357.

358.

Hersch, Martin. Effect of Interchanging Propellants on Rocket Combustor

Performance With Coaxial Injection. Report No. NASA-TN-D-2169, Lewis

Res. Center, Cleveland, Ohio, February 1964.

. Performance and Stability Characteristics of Nitrogen Tetroxide-

Hydrazine Combustors. Report No. NASA-TN-D-4776, Lewis Res. Center,

Cleveland, Ohio, September 1968, 20 pp.

Hersh, Stuart, Henry M. Frey, and Melvin Gerstein. Combustion Chemistry

and Mixing in Supersonic Flow. Phase I. Dynamic Science, a div. of

Marshall Industries,M_nrovia, Calif., Rept. No. DS-TR-A-69-101, Jan. I0,

1969, 81 pp. Report No. AFOSR 69-0104TR, U.S. Air Force (contract

No. AF 49(638)-1712) (project Nos. 9711-01; 6144501F; 681308).

Heft, J. H., and J. B. Gilstein. IndicaDed Instantaneous Temperatures

of Liquid Rocket Exhausts and Combustion Chambers. Jet Propulsion,

v. 25, No. 3, March 1955, pp. 119-127.

Heubusch, Henry Ph. A Method for Studying Precombustion Reactions of

Liquid Propellants. American Chem. Soc., Div. Fuel Chem., v. I,

preprints, Sept. 3-8, 1961, pp. 235-240.

Heybey, W. H., and S. G. Reed, Jr. Weak Detonations and Condensation

Shocks. J. Applied Phys., v. 26, No. 8, August 1955, pp. 969-974.

Hildenbrand, D. L., and W. P. Reid. Burning Rate Studies.

lation of Experimental Eesults With tile Thermal Model.

March 1958, pp. 195-196.

III. Corre-

Jet Propulsion,

Hildenbrand, D. L., and A. Greenville Whittaker. Burning Rate Studies.

II. Variation of Temperature Distribution With Consumption Rate for

Burning Liquid Systems. J. of Phys. Chem., v. 59, 1955, pp. 1024-1028.

Hirschfelder, J. O., C. F. Curtiss, and Dorothy E. Campbell.

of Flame Propagation. IV. J. of Phys. Chem., v. 57, 1953,

pp. 403-414.

The Theory

Hisatsune, I. C., A. P. McHale, R. E. Nightingale, D. L. Rotenberg, and

Bryce Crawford, Jr. On the Inhibition of the NO-NeO 5 Reaction by NO_.

J. of Chem. Phys., v. 23, 1955, p. 2467.

Hisatsune, I. C., and Leo Zafonte. A Kinetic Study of Some Third-Order

Reactions of Nitric Oxide. J. of Phys. Chem., v. 73, No. 9, September1969, pp. 2980-2989.

Hodgkinson, W. R. E. Some Reactions of Hydrazine Nitrate. J. Soc.

Chem. Ind., v. 32, 1913, pp. 519-520.

[] 11 .I,i i,i U U U Li U U R il 11 U U 1; £ i;

32

359.

360.

361.

362.

363.

364.

365.

366.

367.

368.

369.

370.

371.

Hoffman, R. J., R. O. Wright, and B. P. Breen. Combustion Instability

Prediction Using a Nonlinear Bipropellant Vaporization Model.

Dynamic Scl., Div. of Marshall Industries, Monrovla, Calif., con-

tractors Rept. No. 920, January 1968, 95 pp, Report No. NASA-CR-920

(contract NoB. NAS 7-442) prepared for Lewis Res. Center by Dynamic

Science.

Horton, M. D. Use of the One-Dimensional T-Burner To Study Oscillatory

Combustion. AIAA J., v. 2, No. 6, June 1964, pp. 1112-1118.

Horton, M. D., J. L. Eisel, and E. W. Price. Low-Frequency Acoustic

Oscillatory Combustion. AIAA J., v. I, No. II, November 1963,

pp. 2652-2654. NASA (contract No. W-II, 294-B) and Special Projects

Task Assignment 71402.

Horton, M. D., and M. R. McGie. Particulate Damping of Oscillatory

Combustion. AIAA J., v. I, No. 6, June 1963, pp. 1319-1326.

Houseman, John. OptlmumMixing of Hypergolic Propellants in an Unlike

Doublet Injector Element. Jet Propulsion Lab., California Inst. of

Technology, Pasadena, Calif., NASA (contract No. NAS 7-100), 1970.

Hsu, Yih Yun, and Robert W. Graham. A Visual Study of Two-Phase Flow in

a Vertical Tube With Heat Addition. Report No. NASA-TN-D-1564,

January 1963.

Huebner, A. L. Disintegration of Charged Liquid Jets. J. of Fluid

Mech., v. 38, part 4, 1969, pp. 679-688.

Disintegration of Charged Liquid Jets: Results With Isopropyl

Alcohol. Science, v. 168, No. 3927, April 1970, pp. 118-119.

Huff, Vearl N., Sanford Gordon, and Virginia E. Morrell. General Method

and Thermodynamic Tables for Computation of Equilibrium Composition

and Temperature of Chemical Reactions. Report No. NACA-R-1037, 1951.

Hurrell, Herbert G. Analysis of Injectlon-Velocity Effects on Rocket

Motor Dynamics and Stability. Report No. NASA-TR-R-43, 1959.

Husain, D., and R. G. W. Norrish. The Production of NOs in the Photoly-

sis of Nitrogen Dioxide and of Nitric Acid Vapour Under Isothermal

Conditions. Proc. of the Royal Soc., London, ser. A, v. 273, 1963,

pp. 165-179.

Huson, G., and H. Feigel. Controllable Thrust Chamber Study Program,

Task II, July 15, 1961 to October 15, 1961. Thiokol Chem. Corp.,

Reaction Motors Div., Rept. No. RMD-6004-Q2, NASA, October 1961.

lacobellls, S. F., V. R. Larson, and R. V. Burry. Liquid-Propellant

Rocket Engines: Their Status and Future. J. Spacecraft and Rockets,

v. 4, No. 12, December 1967, pp. 1569-1580.

N U

33

372.

373.

374.

375.

376.

377.

378.

379.

380.

381.

382.

Imber, M. Combustion Instability: Liquid Stream and Droplet Behavior.

Part II. Estimating Primary Liquid Jet Break Up With Heat Transfer

Considerations. Wright-Patterson AFB, Aeronautical Res. Lab., Rept.

No. WADC-TR-59-720 (contract No. AF 33(616)-5163), September 1960.

Ingebo, Robert D. Drop-Size Distributions for Impinging Jet Breakup in

Air Streams Simulating the Velocity Conditions in Rocket Combustors.

Report No. NACA-TN-4222, March 1958.

lwama, Akira, and Kiroku Yamazaki. Effect of Some Parameters on the

Ignition Delay of Hypergolic Bipropellants. (I) The Variation With

Liquid Temperature, Oxidant Concentration, Subatmospheric Pressure, and

Fuel Consumption. J. Chem. Soc. Of Japan, Ind. Chem. Section, v. 63,

No. ii, 1960, pp. 1879-1883.

Jain, V. K., and N. Ramani. Extinction Criterion of a Monopropellant

Droplet Burning in an Atmosphere of Inerts. AIAA J., v. 7, No. 3,

March 1969, pp. 567-569.

Jaivin, George I. A Momentum-Balance Method for Measuring the Thickness

of Free Liquid Sheets. Jet Propulsion Lab._ California Inst. of Tech-

nology, Pasadena, Calif., Report-No. NASAITR-32-635 (contract

No. NAS 7-100), Aug. 17, 1964.

James, Harry K., Yael Miron, and Henry E. Perlee. Physical and Explo-

sion Characteristics of Hydrazine Nitrate. BuMines Inf. Circ. 8452,

March 1970, 22 pp. NASA (order No. T-39882(G)).

Johnson, Bruce H. An Experimental Investigation of the Effects of Com-

bustion on the Mixing of Highly Reactive Liquid Propellants. Jet Pro-

pulsion Lab., California Inst. of Technology _ Pasadena, Calif., 1965,20 pp. Report No. NASA-TR-32-689 (contract No. NAS 7-100).

Jones, F. T., T. J. Sworski, J. M. Williams. Radiation Chemistry of

Gaseous An_nonia. Part 2. Hydrazine Formation. Trans. of the Faraday

Soc., part I0, No. 538, v. 63, 1967, pp. 2426-2434.

Jones, Howland B., Jr. Transient Pressure Measuring Methods. Transient

Pressure Transducer Design and Evaluation. Princeton Univ., Rept.

No. AER-595b, NASA (NASr-36), February 1962.

Jones, H. B., Jr., R. C. Knauer, J. P. Layton, and J. P. Thomas. Tran-

sient Pressure Measurements in Liquid Propellant Rocket Thrust Cham-

bers. Trans. of the Instrument So¢. of America (ISA), v. 4, No. 2,1965, pp. 116-132.

Jones, Llewellyn H., Richard M. Badger, and Gordon E. Moore. The Infra-

red Spectrum and the Structure of Gaseous Nitrous Acid. J. of Chem.

Phys., v. 19, No. 12, 1951, pp. 1599-1604.

Ii l/ 1/ 11 11 U li li -U !/ U il 11 U 11 11 /g E

34

383.

384.

385.

386.

387.

388.

389.

390.

391.

392.

393.

394.

Jost, A., K. W. Michel, J. Troe, and H. Gg. Wagner. Detonation and

Shock Tube Studies of Hydrazine and Nitrous Oxide. Univ. of Gottingen,

Germany; U.S. Air Force--ARL (contract No. AF 61(514)-1142), September

1963. Report No. USAF-ARL-63-157.

Juran, Warren, and R. Carl Stechman. Ignition Transients in Small Hyper-

golic Rockets. J. Spacecraft, v. 5, No. 3, March 1968, pp. 288-292.

Juran, Warren, and E. B. Zwick. Dissolved Gas and Helmholtz Resonance

in Rocket Injectors. J. Spacecraft and Rockets, v. 6, No. 3, March

1969, pp. 347-349.

Juran, W., E. B. Zwick, and R. L. Moffett. Gas Effects in Attitude Con-

trol Systems. J. Spacecraft, v. 6, No. ii, November 1969,

pp. 1310-1311.

Kahrs, Jack. Combustion Species Sampling--Final Report. Thiokol Chemi-

cal Corp., Denville, N.J., Rept. No. _ 5530-F, U.S. Air Force (con-

tract No. F04611-68-C-0007), 26 references, June 1968, 77 pp. Report

No. AFRPL-TR-68-120.

Kamlet, Mortimer J., and S. J. Jacobs. The Chemistry of Detonations. I.

A Simple Method for Calculating Detonation Properties of C-H-N-O

Explosives. Report No_- _)LTR 67L_6, U.S.-Naval Ordnance-Lab., White

Oak, Silver Spring, Md., August 1967.

Kana, Daniel D., and John F. Gormley. Longitudinal Vibration of a Model

Space Vehicle Propellant Tank. J. Spacecraft, v. 4, No. 12, December

1967, pp. 1585-1591.

Kaplan, C. J. Selection of a Pressurization System for a Storable

Liquid Propellant Rocket Engine. A.R.S.J., v. 31, June 1961,

pp. 786-793. U.S. Air Force (contract No. AF 33(616)-6684).

Kappl, J. J., and R. M. Knox. Altitude Ignition of Hypergolic Bipropel-

iant Rockets. Marquardt Corp., NAA/S and ID, P.O. No. MYJ 7XA-406013,1965-1966.

Kassel, Louis S. The Kinetics of Homogeneous Gas Reactions.

(Book) (Chapter IX Third Order Reactions). The Chemical Catalog Co.,

1932, pp. 165-176.

Kassoy, David R., and Forman A. Williams. Variable Property Effects on

Liquid Droplet Combustion. AIAA J., v. 6, No. I0, October 1968,

pp. 1961-1965.

Kaufman, Frederick, and Verna Fiora. The Diffusion of NeO 4 inCCl4. Bal-

listic Res. Lab., Aberdeen Proving Ground, Maryland, Memo. Rept.

No. 576, Project No. TB3-0110 of the Res. and Devel. Div., Ordnance

Corps, Div. of the Army, December 1951, 13 pp.

35

395.

396.

397.

398.

399.

400.

401.

402.

403.

404.

405.

Ken_ney,P. Analysis of the Sensitivity of Explosive Materials to Ini-tiation by Impact; Various Statistical Methods. Picatinny Arsenal,Dover, N.J., Tech. Memo.No. 1812, April 1968, 16 pp.

Kiselyk, J. MM_/NmlI4Combustion Stability Comparison. ReportNo. AFRPL-TR-69-45,Air Force Rocket Propulsion Lab., Combustion Tech.Section, Liquid Rocket Div., EdwardsAir Force Base, Calif., March1969.

Kissinger, L. W. The Preparation and Properties of Hydrazine Mononi-trate. NOLMemo.10359, U.S. Naval Ordnance Lab., White Oak, SilverSpring, Md. (NOL-37-Re2¢-19-1(a)), July 7, 1949, 4 pp.

Klein, Lothar, and Gunter J. Penzias. Spectral Radiance MeasurementsofModel Rocket Exhaust Gases, at Simulated Altitude, Using a Rapid Scan-ning Spectrometer. Pres. at the AIAA 5th Aerospace Sci. Meeting inNewYork, Paper No. 40 (PR-40), January 1967.

Kling, R. Str_mungund Verbrennung Gruppe I: ZerstEubung undTropfenr_ssenverteilung Mikrofotografische Untersuchungen VonBrennstoffnebeln in BrennKammern(Photomlcrographic Investigation ofFuel Sprays in Combustion Chambers). Brennstoff-Warme-Kraft J.,v. I0, No. 6, June 1958, pp. 257-263.

Knacke, 0., and J. N. Stranski. The Mechanismof Evaporation. Progressin Metal Phys., v. 6 (edited by B. Chalmers and R. King), 1956.

Knight, R. M., and W. H. Nurick. Correlation of Spray Dropsize Distri-bution and Injector Variables. Rocketdyne, a div. of North AmericanRockwell Corp., Interim Rept. No. R-7995, NASA(contractNo. NAS7-726), September 1969, 108 pp.

Knox, Bruce P., and Henry R. Eberle. Propellant Performance Handbook,Volume VII, Part A. N2Od/Aerozine 50. Bell Aerosystems, Rept.No. R-8173-902008, U.S. Air Force (contract No. AF 04(611)-8183),October 1964.

Propellant Performance Handbook, VolumeVII, Part B. N20_/Aerozine 50. Bell Aerosystems, Rept. No. R-8173-902008, U.S. AirForce (contract No. AF 04(611)-8183), October 1964.

Knox, R. M., and D. C. Sund. Effects on Rocket Engine Operation of Dis-solved Gasesin-Propellants. Paper pres. at a Combustion Symp.meet-ing in Denver, Colo., Oct. 19-20, 1965. (See also the 7th Liquid Pro-pulsion Symp. Bull. CPIA Pub. No. 72, V. II, March 1967, pp. 277-286.)

Koepke, J. M. Detonation Reaction Control (Small Impulse Engine).

Honeywell, Inc., Aeronautical Div., Minneapolis, Minn.; AFFDL-TDR-

64-63, Air Flight Dynamics Lab. (contract No. AF 33(657)-I0959), March

1964. Report No. AFFDL-TDR-64-63.

II II -11 II U U II Li lI 11 II U U li 11 li u r,: i;

36

406

407.

408.

409.

410.

411.

412.

413.

414.

415.

416.

Komov, V. F., and Ya. K. Troshin. On the Structure and Mechanism of the

Detonation of Heterogeneous Systems. Doklady Akademii Nauk, SSSR,

Doklady Phys. Chem., v. 62, May-June 1965, pp. 133-135 (Russian pages);

pp. 365-388 (transl. pages).

Koppang, R. R., R. Fogaroli, and D. J. Simkin. Rocket Recombination

Losses With Storable Propellants Using a Multiple Freeze Point Tech-

nique. Chem. Eng. Progress--Symp. Series, v. 60, No. 52, 1964,

pp. 1-7.

Kors, D. L., L. B. Bassham, and R. E. Walker. A Liquid Rocket Perform-

ance Model Based on Vaporization Inter_tions. J. Spacecraft, v. 6,

No. I0, October 1969, pp. 1133-1138.

Kosvic, T. C., and B. P. Breen. Study of Additive Effects on Hydrazine

Combustion and Combustion Stability at High Pressure. Dynamic Sci.,

a div. of Marshall Industries, Monrovia, Calif., Rept. No. SN-III-F;

Report No_AFRPL'TRf69-i2, U.S.-AirBForce-(c0ntract

No. F04611-68-C-0027), November 1969, 60 pp.

Kovitz, A. A. Large-Amplitude Resonant Combustion in Liquid Rocket

Engine Chambers: Some Aspects of Initiation. Jet Propulsion Lab.,

California Inst. of Technology, Pasadena, Calif., Nov. 15, 1969.

Report No. JPL TR-32-1377 (contract No. NAS 7-100).

Kozirev, S. P. On Cumulative Collapse of Cavitation Cavities. Trans.

of the ASME, J. of Basic Eng., v. 90, No. I, March 1968, pp. 116-124.

Krafft, Joseph M. Surface Friction in Ballistic Penetration. J. of

Applied Phys., v. 26, No. I0, October 1955, pp. 1248-1253.

Krascella, N. L. Theoretical Investigation of the Absorption and Scat-

tering Characteristics of Small Particles. United Aircraft Corp.,

East Hartford, Conn. Report No. NASA-CR-210, NASA (contract

No. NASw-847), April 1965, 57 pp.

Kretschmar, George G. The Isothermal Compressibilities of Some Rocket

Propellant Liquids, and the Ratios of the Two Specific Heats. Jet

Propulsion, A.R.S.J., v. 24, No. 3, May-June 1954, pp. 175-179.

Kruse, Howard W., Jane M. Corcoran, and Sol Skolnik. Preparation of

Hydrazine Nitrate and Hydrazine Nitrate-Hydrazine Mixtures. U.S.

Naval Ordnance Test Station, Inyokern, _China Lake, Calif., Tech. Memo.

No. 321, May 28, 1951.

Kumagai, Seiichiro. Combustion of Fuel Sprays. 6th Symp. (Inter-

national) on Combustion, Paper 88, at Yale Univ., New Haven, Conn.,

Aug. 19-24, 1956, pp. 668-674. Pub. by Reinhold Publishing Corp.,

New York, 1957.

II ll li II II II ll U U U II U U 11 11 II K E

37

417. Kushida, Raymond, and John Houseman. Criteria for Separation of Imping-

ing Streams of Hypergollc Propellants. Jet Propulsion Lab., Califor-

nia Inst. of Technology, Pasadena, Calif., Tech. Memo. 33-395; NASA

(contract No. NAS 7-i00), July 15, 1968.

-418_ Ladanyi,-Dezso J., and Riley O. Miller. Comparison of Ignition Delays

of Several Propellant Combinations Obtained With Modified Open-Cup and

Small-Scale Rocket E_ne Apparatus. Report No. NACA-RM-E53D03,

June 16, 1953.

419. Ladanyi, Dezso J., John L. Sloop, Jack C. Humphrey, and Gerald Morrell.

Starting of Rocket Engine at Conditions of Simulated Altitude Using

Crude Monoethylanillne and Other Fuels With Mixed Acid. Report

No. NACA-RM'E50D20, July 19, i950/ 63-pp. >

420. Laderman, A. J., and A. K. Oppenheim. Influence of Wave Reflections on

the Development of Detonation. Phys. of Fluids, v. 4, No. 6, June

1961, pp. 778-782.

421. Initial Flame Acceleration in an Explosive Gas. Proc. Roy Soc.

(London), Set. A, v. 268, 1962, pp. 153-180.

422. Laderman, A. J., P. A. Urtiew, and A. K. Oppenheim. Effect of Ignition

Geometry on Initial Flame Acceleration _n a Spark Ignited Explosive

Gas. Combustion and Flame, v. 6, December 1962, pp. 325-335.

423.

424.

425.

Landis, E. K., W. W. Wharton, Liang-Chi Chang, and G. M. Jones, Jr.

Critical Point Phenomena in Oscillatory Combustion. Chem. Eng. Prog-

ress Symp. Series, v. 60, No. 52, 1964, pp. 39-44. Army Missile Com-

mand, Redstone Arsenal, Ale. (contract No. DA-01-009-ORD-1018).

Lawhead, R. B., and L. P. Combs. Modeling Techniques for Liquid Propel-

lant Rocket Combustion Processes. 9th Symp. (International) on Com-

bustion, at Cornell Univ., Ithaca, N.Y., Aug. 27-Sept. I, 1962,

pp. 973-981. Pub. by Academic Press, New York, 1963. USAF (contract

No. AF 04(647)-672).

Lawyer, B. R. Rocket Engine Fuel Additive Evaluation Program.

Marquardt Corp., Kept. No. PR 3006-4, monthly letter progress rept.,

Aug. 13-Sept. 10, 1965; NASA (contract No. NAS 9-4299), September 1965.

426. Lawyer, B. R., and B. P. Breen. The Effect of Additives on Droplet

Hydrazine Burning. Paper No. 67-482, pres. at the AIAA Third Propul-

sion Joint Specialist Conf., Washington, D.C., July 17-21, 1967. U.S.

Air Force (contract No. AF 04(611)-I1616), July 1967, 3 pp.

427. . Effects of Additives on the Combustion of Hydrazlne. Dynamic

_., a div. of Marshall Industries, Mourovia, Calif., Third Quart.

Rept.; Rept. No. SN-86-9, Feb. I, 1967, 14 pp. U.S.A.F. (contract

No. AF 04(611)-11616).

38

428.

429.

430.

431.

432.

433.

434.

435.

436.

437.

Lawver, B. R., and B. P. Breen. H_ergolic Stream ImpingementPhenomena--Nitrogen Tetroxide/Hydrazine. Dynamic Sci., a div. ofMarshall Industries, Monrovla, Cailf._ Eeport No. NASA-CR-72444

(contract No. NAS 7-467), October 1968, 25 pp.

Lawyer, B. R., E. W. Nadig, E. Tkachenko, and B. P. Breen. A Mathemati-

cal Model of Random Waves Phenomena in Hypergolic Propellant Combus-

tion. Paper No. 67-517, pres. at the AIAA Third Propulsion Joint

Specialist Conf., Washington, D.C., July 17-21, 1967. NASA (contract

No. NAS 7-467), July 1967.

Lawver, B. R., and E. A. Tkachenko. Heat Release Rate for the Liquid

N204/NeH _ Reaction by Somogyi and Feiler's Method. Dynamic Sci., a

div. of Marshall Industries, Monrovia, Calif., Final Rept. No. SN-II4,

Jet Propulsion Lab. (contract No. 952197) (subcontract under NASA

(NAS 7-100)), 1968.

L'Ecuyer, M. R., and S. N. B. Murthy. Energy Transfer From a Liquid to

Gas Bubbles Forming at a Submerged Orifice. Purdue Univ., Lafayette,

Ind., Report No. NASA-TN-D-2547 (NASA grant NsG-140-61), January 1965.

Lee, Donald H. Performance Calculations for Monopropellant Hydrazine

and Monopropellant Hydrazine-Hydrazine Nitrate Mixtures. Jet Propul-

sion Lab., California Inst. of Technology, Tech. Rept. No. TR-32-348,

Dec. 3, 1962, 87 pp. NASA (contract No. NAS 7-100).

A Survey of the Compatibility of Various Materials With Hydra-

zine and Mixtures of Hydrazine, Hydrazine Nitrate, and Water. Jet

Propulsion Lab., California Inst. of Technology, Pasadena, Calif.,

Memo: No. M-20-152, Dec. 22, 1957, 46 pp. U.S. Army--ORDCIT Project

(contract No. DA-04-495-ORD 18).

Lennert, Andrew E. Analysis of Acid Condensation in an Evacuated Cryo-

chamber. Aero-Space Res. Group, Office of Director of Eng., ARO, Inc.,

ARO Project No. 506002, Rept. No. AEDC-TM-61-4; U.S.A.F., Arnold

Engineering Devel. Center (contract No. AF 40(600)-800 S/A 11(60,110)),March 1961.

Levine, D. M., and David A. Dows. Infrared Spectrum of HN 3 and DN3:

Assignment of the Coriolis-Coupled Bending Vibrations. J. of Chem.

Phys., v. 46, No. 3, Feb. I, 1967, pp. 1168-1172.

Levine, R. S. Experimental Status of H_.gh Frequency Liquid Rocket Com-

bustion Instability. 10th Symp. (International) on Combustion, at the

Univ. of Cambridge, Camb.ridge, England, Aug. 17-21, 1964. Pub. by theCombustion Inst., 1965, pp. 1083-1099. NASA.

Levy, Sherman L., and Owen A. Reynolds. Rocket Propellant Performance

Computation Program for the IBM 650 Computer. - Allied Chem. Corp.,

General Chemical Div., Morristown, N.J. U.S. Army,-Redstone Arsenal

(contract No. DA-30-069-ORD-2638), May 16, 1960, 108 pp.

Ii ILl i,f U IJ U L[ U 11 H H U If If H H l: E

39

438.

439.

440.

441.

442.

443.

444 •

445.

446.

447.

448.

449.

Lewis, J D. Some Basic Studies of Liquid Propellant Injection Pro-

cesses. J. of the Royal Aeronautical Soc., v. 68, November 1964,

pp. 743-758.

Studies of Atomization and Injection Processes in the Liquid

Propellant Rocket Engine. Ministry of Aviation, Rocket Propulsion

Estab., Westcott, Buckinghamshire, England, Tech. Memo. No. 241,December 1961.

Lewis, J. D., and D. Harrison. A Study of Combustion and Recombination .

Reactions During the Nozzle Expansion Process of a Liquid Propellant

Rocket Engine. 8th Symp. (International) on Combustion, at the

California Inst. of Technology, Pasadena, Calif., Aug. 28-Sept. 3,

1960. Paper No. 36, pp. 366-374. Pub. by Williams and Wilkins,1962.

Lewis, J. D., and G. Walker. The Apparent Distortion of the Drop-Size

Distribution in a Liquid Spray Analysed by High-Speed Photographs.

Ministry of Aviation, Rocket Propulsion Estab., Westcott, Buckingham-

shire, England, Rept. No. RPE-TN-213, August 1962.

Liberto, Ralph R. Storable Propellant Data for the Titan II Program.

Bell Aerosystems Company, a series of reports for the Bell Company,

sponsored by the Air Force, for a period of time from October 1960 to

March 1963; U.S. Air Force, 1960-1963.

Loving, F. A. Barricading Hazardous Reactions. Industrial and Eng.

Chem., v. 49, No. I0, October 1957, pp. 1744-1746.

Lucien, Harold W. The Preparation and Properties of Nitrosyl Azide.

American Chem. Soc. J., v. 80, September 1958, pp. 4458-4460.

Preparation and Storage Stability of High-Purity Hydrazine. J.

of Chem. and Eng. Data, v. 7, No. 4, 1962, pp. 541-542.

Thermal Decomposition of Hydrazine. J. of Chem. Eng. Data, v. 6,1961, pp. 584-586.

Luperi, M. Investigations of Space Storable Propellants. Thiokol Chem.

Corp., Reaction Motors Div., Rept. No. RMD-6028-F, NASA, March 1963-January 1964.

Lutzky, Morton. Expioslons in Vacuum. Report No. NOL-TR-62-19, Naval

Ordnance Lab., Jan. 15, 1962, 24 pp.

Lynn, Scott, David M. Mason, and W. H. Corcoran. Ionization in Solu-

tions of Nitrogen Dioxide in Nitric Acid From Optical Absorbance

Measurements. Jet Propulsion Lab., Pasadena, Calif., Progress Rept.

No. 20-175, Sept. 4, 1953, 12 pp. U.S. Army ProjeCt ORDCIT (contract

No. DA-04-495-ORD-18).

\

40

450.

451.

452.

453.

454.

455.

456.

457.

458.

459.

460.

461.

Lyshevskiy, A. S. The Coefficient of Free Turbulence in a Jet of Atom-

ized Liquid Fuel. Trudy Novocherkasskogo Politekhnicheskogo Instituta

No. 33/47; NASA, Tech. Transl. No. NASA-TT-F-351, April 1965.

MacCormack, Robert W. Impact Flash at Low Ambient Pressure. Report

No. NASA-TN-D-2232, Ames Res. Center, Moffett Field, Calif., March

1964, 19 pp.

MacLean, D. I., and _. Gg. Wagner. The Structure of the Reaction Zones

of Ammonia-Oxygen and Hydrazine-Decomposition Flames. llth Symp.

(International) on Combustion, at the Univ. of California, Berkeley,

Calif., Aug. 14-20, 1966, pp. 871-878. Pub. by Combustion Inst., 1967.

Magarvey, R. H., and L. E. Outhouse. Note on the Break-Up of a Charged

Liquid Jet. J. of Fluid Mech., v. 13, 1962, pp. 151-157.

Male, Theodore, and William R. Kerslake. A Method for Prevention of

Screaming in Rocket Engines. Report No. NACA-RM-E54F28a, Lewis Flight

Propulsion Lab., Cleveland, Ohio, Aug. 19, 1954, 23 pp.

Mani, J. V. S. Prediction of Dropsize in Liquid Fuel Sprays. Indian

J. of Technology, v. 7, No. 2, February 1969, pp. 46-49.

Manning, W. P., and W. H. Ganvin. Heat and Mass Transfer To Decelerat-

ing Finely Atomized Sprays. A.I.Ch.E.J., v. 6, June 1960,

pp. 184-190.

Markels, M., Jr., R. Friedumn, and W. Haggerty. A Study of Extinguish-

ment and Control of Fires Involving Hydrazine-Type Fuels With Air and

Nitrogen Tetroxide. Atlantic Res. Corp., Alexandria, Va., Fifth

Quart. Progress Rept., Dec. i, 1960-Feb. 28, 1961, 33 pp. U.S.A.F.

(contract No. AF 33(616)-6918).

Markels, M., Jr., R. Friedman, W. Haggerty, and E. Dezubay. A Study of

Extinguishment and Control of Fires Involving Hydrazine-Type Fuels

With Air and Nitrogen Tetroxide. Atlantic Res. Corp., Alexandria, Va.,

USAFSC-ASD Rept. No. ASD-TR-61-716, May 1962.

Martinkovic, Paul J. Space Vehicle Hazards. AFRPL, Res. and

Tech. Div., AFSC, Edwards. Air Force Base, Calif., Tech. Memo.

AFRPL-TM-64-60, Project 6753, December 1964.

Space Vehicle Propulsion Compartment Fire Hazard Investigation,

Volume I. Air Force Rocket Propulsion Lab., Res. and Tech. Div., AF

Systems Co_mmnd, Edward AFB, Calif., Tech. Document Rept.

No. AFRPL-TDR-64-103, Project No. 6753, Task No. 675303; July 1964.

. Space Vehicle Propulsion Compartment Fire Hazard Investigation,

Volume II. Air Force Rocket Propulsion Lab., Res. and Tech. Div., AF

Systems CoDm_and, Edwards AFB, Calif., Tech. Documentary Rept.

No. AFRPL-TDR-64-170, Project No. 6753, Task No. 675303, December 1964.

IJ lJ ]J LI U U L[ U IJ LI L! L[ . M ]; L ;;

41

462.

463.

464.

465.

466.

467.

468.

469.

470.

471.

472.

Mason, David M., Keith Booman, and Gerard W. Elverum, Jr. Heats of Solu-

tion of Nitrogen Dioxide in the Nitric Acid-Nitrogen Dioxide System at

0 ° C. Jet Propulsion Lab., California Inst. of Technology, Pasadena,

Calif., Progress Rept. No. 20-216, Jan. 29, 1954, 16 pp. U.S. Army

ORDCIT Project (contract No. DA-04-495-Ord 18).

Mason, David M., Ira Petker, Stephen P. Vango. Viscosity and Density of

the Nitric Acid-Nitrogen Dioxide-Water System. Jet Propulsion Lab.,

Progress Rept. No. 20-214, Jan. 29, 1954, 35 pp. U.S. Army ORDCIT

Project (contract No. DA-04-495-Ord 18).

Mayer, E. Vaporization Rate Limited Combustion in Bipropellant Rocket

Chambers. A.R.S.J., v. 29, July 1959, pp. 505-513.

Mayer, S. W., D. Taylor, and L. Schieler. Preignition Products From

Propellants at Simulated High-Altitude Conditions. Combustion Sci.

and Technology, v. i, 1969, pp. 119-129.

Preignition Products From Storable Propellants at Simulated High-

Altitude Conditions. Aerospace Corp., Aerodynamics and Propulsion

Res. Lab., Rept. No. TR-0158(9210-02)-I, November 1967, 44 pp. Space

and Missile Systems Organization, Air Force Systems Command, Los

Angeles Air Force Station, Los Angeles, Calif., Rept.No. SAMSO-TR-68-67.

McAlevy, Robert F., III, and Richard S. Magee. A Criterion for Space

Capsule Fire Hazard Minimization. J. Spacecraft, v. 4, No. i0,

October 1967, p. 1390.

McAuslan, J. H. L. Ignition of Explosives by Light. Proc. of the Royal

Soc. (London), Ser. A, Mathematical and Phys. Sci., v. 246, July-

August 1958, pp. 248-253.

McClure, F. T., R. H. Cantrell, and R. W. Hart. Theoretical Considera-

tions Relating to the Effect of Injector Design on Unstable Burning of

Liquid Propellant Rocket Motors. AIAA J., v. 4, No. i, January 1966,

pp. 84-91.

McCormack, P. D., L. Crane, and S. Birch. An Experimental and Theoreti-

cal Analysis of Cylindrical Liquid Jets Subjected to Vibration.

British J. of Applied Phys., v. 16, No. 3, March 1965, pp. 395-408.

McCullough, Foy, Jr., and H. P. Jenkins, Jr. Studies of the Rates o_

Combustion of Hypergolic Fluids. 5th Symp. (International) on Combus-

tion, at the Univ. of Pittsburgh, Pittsburgh, Pa., Aug. 30-Sept. 3,

1954, Paper No. 9, pp. 181-190. Pub. by Reinhold Publishing Corp.,

New York, 1955.

Mclvor, J. H. Testing Manual, Ballistic Mortar Test. Picatinny Arsenal,

U.S. Army, Memo. No. PAM-7, May 8, 1950.

42

473.

474.

475.

476.

477.

478.

479.

480.

481.

482.

483.

484.

McHale, E. T., B. E. Knox, and H. B. Palmer. Determination of theDecomposition Kinetics of Hydrazine Using a Single-Pulse Shock Tube.lOth Symp. (International) on Combustion, at the Univ. of Cambridge,Cambridge, England, Aug. 17-21, 1964, pp. 341-351; Pub. by the Combus-tion Inst., 1965. Supported in part by Army Res. Office, Durham, andin part by Project Squid under O.N.R. (contractNo. Nonr 1858(25)NR-098-038).

McLain, William H. Combustion Dynamics in Liquid Rocket Engines.Denver Res. Inst., NASA(contract No. NAS9-7566), a series ofmonthly reports, 1968-1970.

McMillan, J. A. Hydrazine-l,l-Dimethylhydrazine Solid-Liquid PhaseDiagram. J. of Chem.and Eng. Data, v. 12, No. I, January 1967,pp. 39-40.

Mead, G. A. Compression Sensitivity of Monopropellants. A.R.S.J.,v. 29, 1959, pp. 192-198.

Ignition Delay Measurement. Air Reduction Company,1962, 37 pp.Air Force SystemsCommand(contract No. AF 04(611)-7413).

Relation of Droplet Consumption Rates to Liquid Strand Consump-tion Rates. A.R.S.J., v. 29, June 1959, pp. 440-442.

M_dard, Louis. Propri_t_s Explosives du Nitrate d'Hydrazine (ExplosiveProperties of Hydrazine Nitrate). M_morial des Poudres, v. 34, 1952,pp. 147-157.

Merrington, A. C., and E. G. Richardson. The Break-Up of Liquid Jets.Proc. of the Phys. Soc., v. 59, part I, No. 331, Jan. i, 1947.

Michaeli, E., and S. Lazerus.Hydrazine Propulsion System.1970, pp. 155-161.

Controlling Initial Pressure Peaks in aIsrael J. of Technology, v. 8, Nos. 1-2,

Michel, K. W., and H. Gg. Wagner. The Pyrolysis and Oxidation of Hydra-zinc Behind ShockWaves. 10th Symp. (International) on Combustion, atthe Univ. of Cambridge, Cambridse, England, Aug. 17-21, 1964,pp. 353-364. Pub. by the Combustion Inst., 1965.

Miesse, C. C. On the Combustion of a Liquid Fuel Spray. 6th Symp.(International) on Combustion, paper No. 96, at Yale Univ., NewHaven,Conn., Aug. 19-24, 1956, pp. 732-738. Pub. by Reinhold Publishing

Corp., New York, 1957.

Correlation of Experimental Data on the Disintegration of Liquid

Jets. Industrial and Eng. Chem., v. 47, No. 9, September 1955,

pp. 1690-1701.

\

43

485.

486.

487.

488.

489.

490.

491.

492.

493.

494.

495.

• The Effect of a Variable Evaporation Rate on the Ballistics of_plets. Armour Res. Foundation, Illinois Inst. of Technology,

WADC,U.S. Air Force.

Oscillation of the Flame Front BetweenTwoUnlike Droplets in aBipropellant Liquid System. 5th Symp. (International) on Combustion,Paper No. I0, at the University of Pittsburgh, Pittsburgh, Pa.,Aug. 30-Sept. 3, 1954, pp. 190-195. Pub. by Reinhold PublishingCorp., NewYork, 1955.

A Theory of Spray Combustion. Ind. and Eng. Chem., v. 50, 1958,pp. 1303-1304.

Mignotte, Ph. Etude Thermodynamiqueet Physicochemique des M_langesd'Hydrazine et de Dim_thylhydrazine _ "Asymetrlque (ThermodynamicandPhysicochemical Study of Mixtures of Hydrazine With AssymmetricDimethylhydrazine). Revue de L'Institut Francais du PEtrol, v. 18,Nos. 7 and 8, July-August 1963, 66 pp. (English), 54 pp. (French).

Mikatarian, Ronald R., and Ralph G. Anderson. An Experimental Investi-gation of a Liquid Jet Expelled Into a Vacuum. J. Spacecraft andRockets, v. 3, No. 2, February 1966, pp. 267-268.

Mill_n, G. Combustion of Sprays, Final Report. Inst. Nac. de Tec.Aeronaut. Esteban Terradas, AFOSRReport No. AFOSR-TR-59-68(contractNo. AF 61(514)-997), Feb. 25, 1959, 9 pp.

Mill_n, G., I. Da Riva, and S. Sanz. Combustion of Fuel Sprays. Inst.

Nac. de Tec. Aeronaut. Esteban. Terradas, AFOSR Report

No. AFOSR-TN-59-629 (contract No. AF 61(514)-997), Jan. 31, 1959, 27 pp.

Millen, D. J., and D. Watson. The Ionisation of Dinitrogen Tetroxide in

Nitric Acid. Evidence From Measurements of Infrared Spectra and Mag-

netic Susceptibilities. J. of the Chem. Soc. (London), January-March

1957, pp. 1369-1372.

Miller, Riley O. Effects of Nitrogen Tetroxide and Water Concentration

on Freezing Point and Ignition Delay °f Fuming Nitric Acid. Report

No. NACA-RM-E53G31, Lewis Flight Propulsion Lab., Cleveland, Ohio,

Sept. 24, 1953, 32 pp.

. Ignition Delays and Fluid Properties of Several Fuels and Nitric

Acid Oxidants in Temperature Range From 70° to -105 ° F. Report

No. NACA-TN-3884, Lewis Flight Propulsion Lab., Cleveland, Ohio,

December 1956.

Low-Temperature Ignition Delay Characteristics of Several Rocket

Fuels With Mixed Acid in Modified Open,Cup-Type Apparatus. Report

No. NACA-RM-ESOHI6, Lewis Flight Propulsion Lab., Cleveland, Ohio,

Res. Memo., Oct. 17, 1950.

I/ I/ 1/ 1I U II U L U U If 1I U 11 11 1/ 11 1: E

44

496.

497.

498.

499.

500.

501.

502.

503.

504.

505.

506.

507.

Milligan, Dolphus E., Harmon W. Brown, and George C. Pimentel. Infrared

Absorption by the N3 Radical. J. of Chem. Phys., v. 25, 1956, p. 1080.

Milligan, Lowell H. The Quantitative Determination of Reduction Prod-

ucts of Free Nitric Acid Solution: Namely--Nitrogen Peroxide, Nitric

Oxide, Nitrous Oxide, Nitrogen, Nitrous Acid, and Salts of Hydroxyl-

amine, Hydrazine, and Ammonia. J. of Phys. Chem., v. 28, 1924,

pp. 544-578.

Mills, T. R., and B. P. Breen. Computer Modeling of Rocket Engine Igni-

tion Transients. Dynamic Sci., a div. of Marshall Industries, Irvine,

Calif., Final Report, May 1970, 115 pp. NASA, Jet Propulsion Lab.,

Pasadena, Calif. (contract No. NAS 7-467).

Mills, T. R., B. P. Breen, E. A. Tkachenko, and B. R. Lawver. Transi-

ents Influencing Rocket Engine Ignition and Popping. Dynamic Sci., a

div. of Marshall Industries, Monrovia, Calif. p Interim (14 month)

Rept. No. SN-95E, Apr. 30, 1969, 76 pp. NASA (contract

No. NAS 7-467, Task 6).

Minion, S. J., and E. B. Zwick. Hypergoiic Combustion Initiated at Low

Pressure. Aviation Space Conf. of the American Soc. of Mech. Eng.,

Los Angeles, Calif., Mar. 16, 1965, 48 pp.

Mitchell, A. H., and H. A. Kirshner. Compression-lgnition Studies of a

Liquid Monopropellant. AZAA J., v. I, No. 9, September 1963,

pp. 2083-2087.

Mitchell, Charles E., Luigi Crocco, and William A. Sirignano. Nonlinear

Oscillations in Liquid Rocket Combustion Chambers. Astronautica Acta

(Pergamon Press), v. 14, 1969, pp. 409-410.

Miyagishima, T. Investigation of High Strain Rate Behavior of Refrac-

tory Alloys and Coatings. The Marquardt Corp., Van Nuys_ Calif.,

Final Rept. No. PR-3OOg-F, February 1966, 212 pp. NASA (contract

No. NAS 9-4905; Project 3009; NASA Accession No. N66-22355 (CR-65319)).

Miyama, Hajime. Kinetic Studies of Ammonia Oxidation in Shock Waves.

IV. Comparison of Induction Periods for the Ignition of NHs-O2-NmWith

Those for NKs-O_-Ar Mixtures. Bull. of the Chem. Soc. of Japan,

v, 41, August 1968, pp. 1761-1765.

Moberly, William H. Shock Tube Study of Hydrazine Decomposition. J.

Phys. Chem., v. 66, T962, pp. 366-368.

Monchick, Louis, and Howard Reiss. Studies of Evaporation of Small

Drops. J. of Chem. Phys., v. 22, No. 5, May 1954, pp. 831-836.

Moore, Gordon E. The Spectrum of Nitrogen Dioxide in the 1.4-3.4_

Region and the Vibrational and Rotational Constants of the NO_ Mole-

cule. J. of the Optical Soc. of America, v. 43, No. II, November

1953, pp. 1045-1050.

45

508.

509.

510.

511.

512.

513.

514.

515.

516.

517.

518.

519.

Moran, H. E., Jr., J. C. Burnett, and E. I. Smith, Jr. ExplosionHazards of Mixed Hydrazine Fuel. U.S. Naval Res. Lab., Eng. Res.Branch, Mech. Div., Washington, D.C., NRLMemo.Rept. No. 1615, May1965, 13 pp.

Morrell, Gerald. Critical Conditions for Drop and Jet Shattering.Report No. NASA-TN-D-677,Lewis Res. Center, Cleveland, Ohio,February 1961.

Rate of Liquid Jet Breakup by a Transverse Shock Wave. ReportNo. NASA-TN-1728,Lewis Res. Center, Cleveland, Ohio, May 1963.

. Summary of NACA Research on Ignition Lag of Self-Igniting Fuel-

Nitrlc Acid Propellants. Report No. NACA-RM-E57GI9, Oct. 3, 1957.

Morrell, Gerald, and Frederick P. Povinelli. Breakup of Various Liquid

Jets by Shock Waves and Applications to Resonant Combustion. Report

No. NASA-TN-D-2423, August 1964.

Mouritsen, T. E., and C. E. Sullivan. Small Liquid Propulsion Systems

Testing in a Space Envirom_ent Simulator. J. of Spacecraft and

Rockets, v. 4, No. 5, May 1967, pp. 687-689.

Moutet, H., A. Moutet, and M. Barr_re. Les Conditions D'Allumage des

Propergols a l'Etat Liquide et Gazeu_. Influence de la Pression et

de la Temperature (Conditions of Ignition of Propergols in the Liquid

and in the Gaseous States. Effect of Pressure and Temperature). Revue

De L'institut Francais Du P_trole, v. 13, No. 4, April 1958.

Muraca, R. F., J. S. Whituick, and C. A. Crutchfleld. The Results of

Long-Term Storage Tests for Compatib_llties of Spacecraft Materials

With Hydrazine and Hydrazine Mixtures. Jet Propulsion Lab., Califor-

nia Inst. of Technology, JPL contract No. 951581, SRI Rept.

No. 951581-6, SRI Project ASD-6063; NASA (contract No. NAS 7-100),October 1967.

Muraca, R. F., Edward Willis, C. H. Martin, and C. A. Crutchfield.

Determination of Water in Nitrogen Tetroxide: Gas Chromatographic

Method for Total Hydrogen Content. Analytical Chem., v. 41, No. 2,

February 1969, pp. 295-298.

Murray, R. C., and A. R. Hail. Flame Speeds in Hydrazine Vapour and in

Mixtures of Hydrazine and Ammonia With Oxygen. Trans. Faraday Soc.,

v. 47, 1951, pp. 743-751.

Musslewhlte, Robert C., Jr. Handling Dangerous Materials in Confined

Areas. Northrup Space Labs., Rept. No. NSL 64-244, September 1964,

18 pp.

Nachbar, William. Deflagration Lim/ts in an Adiabatic Model for Steady

Linear Burner of a Monopropellant. AIAA J., v. 7, No. 8, August 1969,

pp. 1593-1598.

46

520.

521.

522.

523.

524.

525.

526.

527.

528.

Nachtsheim, PhilipR. Analysis of the Stability of a Thin Liquid FilmAdjacent to a High SpeedGas Stream. Report No. NASA-TN-D-4976,AmesRes. Center, Moffet Field, Calif., January 1969.

Nadig, E. W., B. R. Lawver, and B. P. Breen. A Study of RandomWavePhenomenain Hypergolic Propellant Combustion. Dynamic Sci. Corp.,Monrovia, Calif., Semi-annual Report, Rept. No. SN-87-6, NASA,Nov. 30, 1966, 20 pp.

Naphtali, Leonard M., and SamuelZ. Burstein. Evaporation and Breakupof Fuel Droplets in OneDimensional Gas Flow in a Combustion Chamber.Polytechnic Inst. of Brooklyn, AFOSRReport No. AFOSR-TN-60_229(contract No. AF 49(638)-165, Project No. 9751), January 1960.

Newton, AmosS., and A. F. Sciamanna. Metastable Peaks in the MassSpectra of NmOand NO_. J. of Chem.Phys., v. 44, No. ii, June 1966,pp. 4327-4332.

Nicholls, J. A. TwoPhase Detonation as Related to Rocket Motor Combus-tion Instability. Gas Dynamic Lab., Univ. of Michigan, Ann Arbor,Mich., Rept. No. UM-06324-6-F, February 1969, 26 pp. ReportNo. NASACR-72532; NASA(contract NO. NASr 54(07)).

Nicholls, J. A., R. E. Cullen, T. C. Ad_nson, G. L. Cosens, M. Sichel,E. Kurath, F. Cheslak, G. Olsson, J. Fu, T. David, J. Brown,K. Ragland, and S. Schmidt. The Feasibility of a Rotating DetonationWaveRocket Motor. Univ. of Michigan_ Dept. of Aeronautical andAstronautical Eng., Aircraft Propulsion Lab., Ann Arbor, Mich., Rept.No. 05179-2-P; Quart. Progress Rept. No. 2 (Sept. 1-Nov. 30, 1962).Air Force Flight Test Center, EdwardsAir Force Base, Calif. (contractNo. AF 04(611)-8503), December1962.

Nicholls, J. A., R. E. Cullen, G. L. Cosens, M. Sichel, E. Kurath,F. Cheslak, G. Olsson, J. Fu, T. David, J. Brown, and K. Ragland. TheFeasibility of a Rotating Detonation WaveRocket Motor. Univ. ofMich., Dept. of Aeronautical and Astronautical Eng., Aircraft Propul-sion Lab., Ann Arbor, Mich., Rept. No. 05179-I-P; Quart. ProgressRept. No. I (June 1-Aug. 31, 1962), 45 pp. Air Force Flight TestCenter, EdwardsAir Force Base, Calif. (contract No. AF 04(611)-8503),August 1962.

Nicholls, J. A., R. E. Cullen, G. Olsson, G. L. Cosens, K. Ragland,J. Brown, S. Schmidt, E. Kurath, and F. Cheslak. The Feasibility of a

Rotating Detonation Wave Rocket Motor. Univ. of Michigan, Office of

Res. Admin., Dept. of Aeronautical and Astronautical Eng., Aircraft

Propulsion Lab., Ann Arbor, Mich., ORA Project 05179-4-P; Quart. Prog-

ress Rept. No. 4 (Mar. 1-May 31, 1963), 31 pp. Air Force Flight Test

Center, Edwards Air Force Base, Calif. (contract No. AF 04(611)-8503),

June 1963.

Nicholls, J. A., E. K. Dabora, and K. W. Ragland. A Study of Two-Phase

Detonation as It Relates _to Rocke_t Moto K Combustion Instability. Univ.

of Michigan, Report No. NASA-CR-272; NASA (contract No. NASr-54(07)),

August 1965.

11 U 11 1I lI U 11 11 11 IJ 11 il ii 11 g LIi I/ _ILl

47

529.

530.

531.

532.

533.

534.

535.

536.

537.

538.

539.

540.

Eightingale, R. E., A. R. Dow_ie, D. L. Rotemberg, Bryce Crawford, Jr.,

and R. A. Ogg, Jr. The Preparation and Infrared Spectra of the Ox±de_

of Nitrogen. J. of Phys. Chem., v. 58, 1954, pp. 1047-1050.

Nishiwak, Niichi. Kinetics of Liquid Combustion Processes; Evaporation

and Ignition Lag of Fuel Droplets. 5th Symp. (International) on Com-

bustion, Paper No. 5, at the Univ. of Pittsburgh, Pittsburgh, Pa.,

Aug. 30-Sept. 3, 1954. Pub. by Reinhold Publishing Corp., New York,

1955, pp. 148-158.

Nordberg, William. Acoustic Phenomena Observed on Rocket-Borne High

Altitude Explosions. Report No. NASA-TN-D-1294, June 1962.

Norrish, R. G. W. The Kinetics and Analysis of Very Fast Chemical

Reactions. Chem. in Britain, v. i, No. 7, July 1965, pp. 289-311.

Nurick, W. H., and S. D. Clapp.

ment of Injector Spray Mixing.

1969, pp. 1312-1315.

An Experimental Technique for Measure-

J. Spacecraft, v. 6, No. Ii, November

Nussle, Ralph C., Joseph D. Derdul, and Donald A. Petrash. Photographic

Study of Propellant Outflow From a Cylindrical Tank During Weightless-

ness. Report No. NASA-TN-D-2572, February-i965.

O'Brien, Arthur W., and Charles L. Caudill. Design and Fabrication of

Hydrazine Storability Test Tanks. Martin Marietta Corp., Final Rept.,

U.S. Air Force, Report No. AFRPL-TR-69-iI2, June 1969.

Oppenheim. A. K. Novel Insight Into the Structure and Development of

Detonation. Astronautica Acta, v. Ii, No. 6, 1965, pp. 391-400.

USAF AFSOR (contract No. AF-129-65) and NASA (grant

No. NsG-702-05-003-050).

Oppenheim, A. K., and R. A. Stern. Development and Structure of Plane

Detonation Waves. Univ. of California, Report No. AFOSR-TN-60-124,January 1960.

Oppenheim, A. K., R. A. Stern, and P. A. Urtlew. On the Development of

Detonation With Pre-ignitlon. Combustion and Flame, v. 4, 1960,pp. 335-341.

Osborn, J. R., and L. R. Davis. Effects of\Injection Location on Com-

bustion Instability in Premixed Gaseous Bip_pellant Rocket Motors.Purdue Univ., Jet Propulsion Center, Rept._. 1-61-1, Office of Naval

Res., January 1961.

Osborn, J. R., and D. W. Netzer. Parametric Study of Rocket Instability(Final Report 11/1/65 to 1/31/68). PurdUe Univ., School of Mech.

Eng., Lafayette, Ind., AFOSR (contract No. AFOSR 753-66), Feb. 15,1968.

Ii I1 il 11 11 1I tl 1I U U II U 11 11 i1 U g iX I;

48

541.

542.

543.

544.

545.

546.

547.

548.

549.

550.

551.

Osborn, J. R., and R. M. Schieve. An Experimental Investigation of High

Frequency Combustion Pressure Oscillations in a Gaseous Bipropellant

Rocket Motor. Purdue Univ., Jet Propulsion Center, Lafayette, Ind.,

Rept. No. 1-58-1, Office of Naval Res. (contract No. N7 Ord-39418),

June 1958.

• °

Pannetier, Guy, and Maurice Lecamp. Sur l'exlstence d'une limite

inferieure de pression dans la decomposition explosive de l'acide

azothydrique sous l'influence de l'_tincelle _lectrique. Influence degas estrangers (On the Existence of a Lower Pressure Limit in the

Explosive Decomposition of Hydrazoic Acid Under the Influence of an

Memolres Pr_sentes aElectric Spark. Influence of Foreign Gases). • "

la Societe Chlmique, 1954, pp. 1068-1070.

Pannetier, Guy, and Philippe Mignotte. Equilibre liquide-vapeur du

binaire hydrazine-dimethylhydrazine asym_trique (Liquid-Vapor Equilib-

rium in the Binary System N_H4-UDMII). Bull. Soc. Chim. France, Paper

No. 143, 1961, pp. 985-988.

Pannetier, G., Ph. Mignotte, and M. Chevillon. Inhibition de l'autod_-

composition de l'acide azothydrique (]inhibition of the Autodecomposi-

tion of Hydrazoic Acid). Soc. Chim. France, Bull. No. 154, 1960,

pp. 804-807.

Pannetier, Guy, Philippe Mignotte, and Maurice Dode. Binary Mixture

Hydrazine-UDMH. IV. Thermodynamic Study: Molecular Associations.

Bull. Soc. Chim. France, Paper No. 299, 1963, pp. 1834-1837.

Papazian, Harold A. The Decomposition of Solid H4N e Induced by Charged

Particle Bombardment. J. of Phys. ChemL., v. 65, January 1961,

pp. 53-55.

Nitrogen Chained Compounds as Intermediates in the Photolysis of

Solid HN 3. J. of Chem. Phys., v. 32, No. 2, February 1960,

pp. 456-460.

Papazian, Harold A., and Angelo P. Margozzi. On the Photolysis of Solid

HNs. J. of Chem. Phys., v. 44, No. 2, 1966, pp. 843-844.

Patry, Marcel, Robert Garlet, Samuel Pupko, and Paul Pascal. Chimie

Minerale--Sur les reactions entre les oxydes d'azote et l'ammoniac

(Inorganic Chemistry--Reactions Between Nitrogen Oxides and Ammonia).

Academic Des Science, Paris Comptes Rendus, v. 225, 1947, pp. 941-942•

Paushkin, Ya. M. The Chemistry of Reaction Fuels. Institute

Neftekhimicheskogo Sinteza; Wright-Patterson AFB, Foreign Technology

Div., Transl. Rept. No. FTD-TT-62-1417, Nov. 8, 1962.

Penneman, R• A., and L. F. Audrieth. Quantitative Determination of

Hydrazine. Analytical Chem., v. 20, No. ii, November 1948,pp. 1058-1061.

IJ 11 il ]U 1; 11 1; U U U_ U U 11 11 U ;; E i;

49

552.

553.

554.

555.

556.

557.

b _8.

559.

560.

561.

Penner, Stanford S. Quantitative Evaluation of Rocket Propellants.

American J. of Phys., v. 20, No. i, January 1952, pp. 26-31.

Penner, S. S., and P. P. Darner. Combustion Problems in Liquid-Fuel

Rocket Engines. 5th Symp. (International) on Combustion, Paper III,

at the Univ. of Pittsburgh, Pittsburgh, Pa., Aug. 30-Sept. 3, 1954,

pp. 11-29. Pub. by Reinhold Publishing Corp., New York, 1955. Sup-

ported in part by U.S. Army, Office of Ordnance Res. (contract

No. DA 04-495-Ord-446 with California Inst. of Technology) and in part

by USAFOSR, Air Res. and Devel. Command (contract No. AF 18(600)-799

with Aerojet-General Corp.).

Penner, S. S., and A. E. Fuhs.

Liquid-Fuel Rocket Engines.

pp. 229-240.

On Generalized Scaling Procedures for

Combustion and Flame, v. I, 1957,

Penney, W. G., and G. B. B. M. Sutherland. A Note on the Structure of

He O_ and _N_ With Particular Reference to Electric Moments and Free

Rotation. Trans. of the Faraday Soc., v. 30, 1934, pp. 898-903.

Pe_ez del Notario, P., and C. Sanchez Tarifa. An Experimental Investi-

gation of the Combustion of Monopropellants Droplets. Instituto

National de Tecnica Aeronautica; AFOSR Report No. AFOSR-TN-59-628

(contract No_AF-61_51--_L997), through the European Office ARDC,

Jan. 20, 1959, 24 pp.

Perkins, Harold. Effects of Various Ad_itlves on Physical Properties

and Performance of Monomethylhydrazine. Report No. NASA-TM-X-53356,

NASA, George C. Marshall Space Flight Center, Huntsville, Ala.,

Nov. 3, 1965.

Perlec, Henry E., Theodore Christos. Stmlnary of Literature Survey of

l{ypu_gollc Ignition Spike Phenomena. BuMines, Pittsburgh, Pa.,

Phase 1--Final Rept. No. 3982, Apr. 8-Dec. 31, 1965, 44 pp. NASA,

Houston, Tex. (order No. T-39882(G)).

Perlee, H. E., T. Christos, Y. Miron, and H. K. James. Preignition

Phenomena in Small A-50/NTO Pulsed Rocket Engines. J. Spacecraft and

Rockets, v. 5, No. 4, February 1968, pp. 233-235.

Perlee, Henry E., Agnes C. Imhof, and Michael G. Zabetakis. Flammabil-

ity Characteristics of Hydrazine-Unsymmetrical Dimethyl Hydrazine-

Nitrogen Tetroxide-Air Mixtures. BuMines, Explosives Res. Center,

Final Rept. No. 3806, Feb. 15, 1961, 17 pp. Bell Aerosystems Company,

Agreement No. 14-09-050-2137.

Flammability Characteristics of Hydrazine-Unsymmetrical

Dimethyl Hydrazine-Nitrogen Tetroxide-Air-Water Mixtures. BuMines,

Explosive Res. Center, Rept. No. 3844; Supplementary to Final Rept.

No. 3806, Dec. 12, 1961, 14 pp. Bell Aerosystems Company, AgreementNo. 14-09-050-2137.

50

562.

563.

564.

565.

566.

567.

568.

569.

570.

571.

Perlee, Henry E., Agnes C. Imhof, and Michael G. Zabetakis. Flammabil-ity Characteristics of Hydrazine Fuels in Nitrogen Tetroxide Atmos-pheres. J. of Chem.and Eng. Data, v. 7, No. 3, July 1962,pp. 377-379.

Perlee, H. E., E. L. Litchfield, J. C. Cooper, C. M. Mason, andM. G. Zabetakis. Fire, Explosion and Handling Hazards of Titan IIMissile Fuel. BuMines, Final Rept. No. 3880, Feb. 15, 1963, i0 pp.Ballistics Systems Div., Air Force Systems Command(orderNo. (04-694) 62-56).

Perlee, Henry, and Yael Miron. Hypergolic Ignition and CombustionPhenomenain the Propellant SystemAerozine-50/N204. BuMines, Pitts-burgh, Pa., Quart. Rept. No. 4086, Dec. I, 1968-Mar. 31, 1969, 12 pp.NASA,Houston, Tex. (order No. T-39882(G)), 1969.

Perlee, Henry E., Yael Miron, and Harry James. Hypergolic Ignition andCombustionPhenomenain the Propellant System Aerozine-50/NmO4 .BuMines, Pittsburgh, Pa., Quart. Rept., June 1-Aug. 31, 1967, 5 pp.NASA,Houston, Tex. (order No. T-39882(G)), 1967.

Hypergolic Ignition and Combustion Phenomenain the PropellantSystemAerozine-50/N_O4. BuMines, Pittsburgh, Pa., Ann. Rept.No. 4071, Sept. i, 1967-Nov. 30, 1968, 9 pp. NASA,Houston, Tex.(order No. T-39882(G)), 1968.

Reply by Authors to C. W. Baulknight's Commentson '_reignitionPhenomenain Small A-50/NTO Pulsed Rocket Engines." J. Spacecraft andRockets, v. 5, No. 8, August 1968, p. 1008.

Perlee, Henry E., Yael Mi_on, Harry James, and Theodore Christos. Hyper-golic Ignition and Combustion Phenomenain the Propellant SystemAerozine-50/NmO4 . BuMines, Pittsburgh, Pa., Final Rept. No. 4019,Apr. I, 1965-Mar. 31, 1967, 40 pp. NASA,Houston, Tex. (orderNo. T-39882(G)), 1967.

Perry, Cortes L., and E. D. Coon. A Spectrophotometric Study of theDissociation of Dinitrogen Tetroxide. Proc. of North Dakota Academyof Sci., v. XIII, 1959, 6 pp.

Pesante, R. E., M. Nishibayashi, and D. G. Frutchey. Blast and FireballComparison of Cryogenic and Hypergolic Propellants. Aerojet GeneralCorp., Downey,Calif., Rept. No. 0822-01(0_ FP; NASA (MSC) (contract

No. NAS-9-2055), June 1964.

Pieper, J. L., L. E. Dean, and R. S. Valentine. Mixture Ratio Distribu-

tion--Its Impact on Rocket Thrust Chamber Performance. J. Spacecraft,v. 4, No. 6, January-June 1967, pp. 786-789.

Ii _11 U U U 13 U U U U U U U n U g il

51

572.

573.

574.

575.

576.

577.

578.

579.

580.

581.

582.

583.

584.

Pimentel, George C., Stuart W. Charles, and Kjell Rosengren. Hydrogen

Bonding of Hydrazoic Acid in Solid Nitrogen. J. of Chem. Phys., v. 44,

No. 8, Apr. 15, 1966, pp. 3029-3033.

Pino, M. A. A Versatile Ignition Delay Tester for Self-lgniting Rocket

Propellants. Jet Propulsion, v. 25, September 1955, pp. 463-466.

Pittaway, Alan R. Investigation of the Flashing of Aerosols. Midwest

Res. Inst., Quart. Progress Rept. No. i, Dept. of the Army, July 25,

1963.

Pollard, F. H., and P. Woodward. Reactions Between Formaldehyde and

Nitrogen Dioxide. Part II. The Explosive Reaction. Trans. Faraday

Soc., v. 45, No. 320, Part 8, August 1949, pp. 767-770.

Pollard, F. H., and R. M. H. Wyatt. Reactions Between Formaldehyde and

Nitrogen Dioxide. Part I. The Kinetics of the Slow Reaction. Trans.

Faraday Soc., v. 45, No. 320, Part 8, August 1949, pp. 760-767.

Popov, Mintscho. Modellversuche mit Fl_ssigkeitszerst_ubung (Mode_Experiments on Atomization of Liquids). Acad. Rep. Populare Romane,

Rev. de Mecanique Ap-pliqu_e-f v. _,-N-o.-l, 1-956, pp. 71-88 (Buchares t) ;

NASA Tech. Transl. F-65, July 1961, 33 pp.

Porter, J.W. Pulsating Combustion of Liquid Fuel in Partially Closed

Vessels. Combustion and Flame, v. Ii, 1967, pp. 501-510.

Porter, R. N., B. H. Johnson, W. B. Tyler, and H. B. Stanford. Advanced

Liquid Propulsion Systems. JPL Space Programs Sursnary No. 37-29,

v. IV, October 1964, pp. 100-105.

Powell, Walter B., James P. Irving, and Glen W. Powell. A Method for

the Determination of Local Transient Heat Flux in Uncooled Rocket

Motors. Jet Propulsion Lab., California Inst. of Technology, Report

No. NASA-TR-32-257 (contract No. NAS 7_I00), July I, 1962.

Price, Donna. Contrasting Patterns in the Behavior of High Explosives.

llth Symp. (International) on Combustion, at the Univ. of California,

Berkeley, Calif., Aug. 14-20, 1966. Pub. by the Combustion Inst.,

1967, pp. 693-702.

Price, Donna, T. P. Liddiard, Jr., and R. D. Drosd. The Detonation

Behavior of Hydrazlne Mononitrate. Naval Ordnance Lab., White Oak,

Md., Report No. NOLTR-66-31, Apr. 15, 1966, 15 pp.

Priem, Richard J. Influence of Combustion Process on Stability.No. NASA-TN-D-2957) August 1965. --

Report

Propellant Vaporization as a Criterion for Rocket Engine Design;

Calculatlon_s0f Chmber Length To V apprize Various Propellants.

Report No. NACA-TN-3883, September 1958, 36 pp.

II U .IJ il IJ U U U U U u U u u £ c

52

585.

586.

587.

588.

589.

590.

591.

592.

593.

594.

595.

596.

Priem, Richard J. Propellant Vaporization as a Criterion for the Rocket

Engine Design; Calculations Using Various Log-Probability Distribu-

tions of Heptane Drops. Report No. NACA-TN-4098, October 1957.

Theoretical and Experimental Models for Unstable Rocket Com-

bustor. 9th Symp. (International) on Combustion, at Cornell Univ.,

Ithaca, N.Y., Aug. 27-Sept. I, 1962, pp. 982-992. Pub. by Academic

Press, New York, 1963.

Priem, Richard J., and Marcus F. Heidmann. Propellant Vaporization as a

Criterion for Rocket Engine Design: Relation Between Percentage of

Propellant Vaporized and Engine Performance. Report No. NACA-TN-4219,

March 1958.

Propellant Vaporization as a Design Criterion for Rocket-Engine

Combustion Chambers. Report No. NASA-TR-R-67, 1960.

. Vaporization of Propellants in Kocket Engines. A.R.S.J.,

v. 29, November 1959, pp. 836-842.

Progelhof, R. C. Determination of the Mass of Gas in a Rapidly Dis-

charging Vessel. AIAA J., v. 2, No. I, January 1964, pp. 137-139.

Rabin, E., and R. Lawhead. The Motion and Shattering of Burning and

Nonburning Propellant ,Droplets. Rocketdyne, a div. of North AmericanAviation, Inc.; Report No. AFOSR_TN-5-9-Ji29_AFOSR (contract

No. AF 18(603)198), March 1959.

Rabin, E., A. R. Schallenmuller, and R. B. Lawhead. Displacement and

Shattering of Propellant Droplets: Rocket d___e, a div. of North

American Aviation, In_c.; Report N 9. A_OSR-TR-60-75, AFOSR (contract

No. AF 18(603)-98), March 1960.

Ragland, K. W., E. K. Dabora, and J. A. Nicholls. Shock Induced Hetero-

geneous Detonations. Paper No. WSCI-65-22, pres. at the 1965 Fall

Meeting of Western States Section of the Combustion Inst., October

1965 (Univ. of Michigan; Aircraft Propulsion Lab.). NASA (contract

No. NASr 54 (07)).

Ramsden, G. R. Procedure for the Operation of the MS4 Mass Spectrometer

in the Determination of Local Mixture Ratio in Rocket Engines. Rocket

Propulsion Estab., Westcott, England, Tech. Memo. TM-308, December

1963.

Ranz, W. E., and Clarence Hofelt, Jr. Determining Drop Size Distribu-

tion of a Nozzle Spray. Ind. and Eng. Chem., v. 49, 1957, pp. 288-293.

Rapp, Louis R., and Murray P. Strier. The Effect of Chemical Structure

on the Hypergolic Ignition of Amine Fuels. Jet Propulsion, April 1957,

pp. 401-404.

II II .M IJ U tl -lJ -U II 1,1 ]J II II II IX I,: L

53

597.

598.

599.

600.

Rastogi, R. P., and K. Kishore. Mechanism of Combustion of Liquid

Rocket Propellants: Aliphatic Alcohols and Mixed Acid. AIAA J., v. 4,

No. 6, June 1966, pp. 1083-1085.

Rastogi, R. P., and T. P. Pandya. Composition of Reaction Mixture Flow-

ing Through Rocket Nozzle. A.R.S.J., v. 30, 1960, pp. 63-64, 113.

Ray, A. B., G. Koehler, G. E. Salser, and L. Dauerman. Azides in the

Condensed Phase Reaction Between N_I_/NmO_. Paper No, 1-2, pres. at

the 1969 Tech. Meeting of the Eastern Section of the Combustion Inst.,

Morgantown, W. Va., Sept. 29, 1969.

Evidence for the Formation of Azides in the N_B_/NmO 4 Reaction.

AIAA J., v. 6, No. II_ November 1968, pp. 2186-2187.

601.

602.

603.

604.

605.

606.

607.

608.

Reardon, F. H. Combustion Instability in Liquid Propellant Rocket

Motors. An Investigation of Transverse Mode Combustion Instability in

Liquid Propellant Rocket Motors. Princeton Univ., Aeronautical Eng.

Dept., Princeton, N.J., Rept. No. AER-550, June i, 1961, 213 pp.

Dept. of the Navy, Bureau of Naval Weapons (contract NOas-60-6078-C).

Reba, Imants, and Coleman Brosilow. Combustion Instability: Liquid

Stream and Droplet Behavior. Part Iii. The Response of Liquid Jets

to Large Amplitude Sonic Oscillations. Wright-Patterson AFB, Aero-

nautical Res. Lab.; Wright Air Devel. Center; Report

No. WADC-TR-59-720, USAF (contract AF 33(616)-5163), September 1960.

Redmond, Thomas F., and Bradford B. Wayland. Dimerization of Nitrogen

Dioxide in Solution: A Comparison of Solution Thermodynamics With the

Gas Phase. J. of Phys. Chem., v. 72=. No. 5, May 1968, pp. 1626-1629.

Reichenbach, R., D. Squires, and S. S. Penner. Flame Propagation in

Liquid-Fuel Droplet Arrays. California Inst. of Technology, Rept.

No. TN-30; U.S. Army (contract No. _-04-495-Ord-1634), June 1960.

Ribovich, John. A Wedge Technique for Evaluation of Detonation Hazards

of Liquid Explosives. Annals of the New York Acad. of Sci., v. 152,

art. I, Oct. 28, 1968, pp. 766-772. Bureau of Naval Weapons, U.S.

Dept. of the Navy (Project No. 19-66-8027-WEPS).

Richardson, E. G. Mechanism of the Disruption of Liquid Jets. Applied

Sci. Res., Section A, v. 4, 1954, pp. 374-380.

Richter, G. N., H. H. Reamer, and B. H. Sage. Oxides of Nitrogen in

Combustion: Investigations in a Premixed Flame. Chem. Eng. Sci.,

v. 17, November 1962, pp. 813-823.

Riebling, Robert W. Criteria for Optimum Propellant Mixing in Impinging-

Jet Injection Elements. J. Spacecraft and Rockets, v. 4, No. 6, June

1967, pp. 817-819.

U _U II U li lI U U I! II II 11 11 II 1:

54

609.

610.

611.

612.

613.

614.

615.

616.

617.

618.

619.

620.

621.

Roberts, Leonard, and Jerry C. South, Jr. Comments on Exhaust Flow Field

and Surface Impingement. AIAA J., v. 2, No. 5, May 1964, pp. 971-974.

Robinette, Roy C., Jr. Computer Calculations of Rocket Engine Combus-

tion Properties. Univ. of Wyoming, Thesis for the Degree of Master of

of Sci., Dept. of Mech. Eng. and Graduate School, Laramie, Wyo., May

1963, 62 pp.

Robinson, Robert J., and Walter C. McCrone. Hydrazine Nitrite (1).

Anal. Chem., v. 30, 1958, pp. 1014-1015.

Rodean, Howard C. Rocket Thrust Termination Transients. A.R.S.J.,

June 1959, pp. 406-409.

Rodriguez, S. E., and A. E. Axworthy. Liquid Phase Reactions of Hyper-

golic Propellants. Rocketdyne, a div. of North American Rockwell,

Final Rept. No. 8374; NASA, Jet Propulsion Lab. , Pasadena, Calif.(contract NAS-Y'739_Dec_-I, 1970, 75 pp.

'7

Rollbuhler, R. James, and William A. Tomazic. Comparison of Hydrazine-

Nitrogen Tetroxide andH3drazlne_-Ch!orlne_Trifluoride in Small-Scale

Rocket Chambers. Report No. NASA-TNID-131, October 1959.

Rosen, Gerald. Nonlinear Pressure Oscillations in a Combustion Field.

A.R.S.J., v. 30, 1960, pp. 422-423.

Rosen, J. M. A New Apparatus for the Determination of the Ignition Tem-

perature of Explosives. U.S. Naval Ordnance Lab., White Oak, Silver

Spring, Md. Report No. NOL-Memo-10289 (NOL-37-Re 2C-19-I(a)), Dec. I,1949.

Rosser, Willis A., Jr., and Henry Wise. Thermal Decomposition of Nitro-

gen Dioxide. J. of Chem. Phys., v. 24, 19_6, pp. 493-494. Dept. of

the Army, Ordnance Corps (contract No. DA-04-495-ORD-18).

Rossmann, Theodor G. A High Speed and High Resolution Photographic Tech-

nique for the Observation of Propellants Injected Into a Firing Cbm-

bustion Chamber. Bell Aircraft Corp. Rept. No. 8007-981-008 (contract

No. AF 49(638)-260), May 18, 1959. Report NO. AFOSR-TN-59-8.

Observation of Propellants Injected Into a Firing Rocket Chamber.

Bell Aerosystems Company, Div. of B@II Aerospace Corp., Rept.

No. 8007-981-011 (contract No. AF 49(638)-260), July I, 1960. ReportNo. AFOSR-TR-60-98.

Program of Exploratory Research on Rocket Engine Combustion,

Final Report. Bell Aircraft Corp., Rept. No. R-02-982-026 (contract

No. AF 18(600)-1156), Oct. 15, 1957. Report No. AFOSR-TR-58-17.

Rothberg, Sidney, and Ogle B. Cope. Toxicity Studies on Hydrazine,

Methylhydrazlne, Symmetrical Dimethylhydrazine, Unsymmetrical Dimeth-

ylhydrazlne and Dimethylnitrosamine. Chem. Warfare Lab., Rept.

No. 2027 (Project No. 4-61-14-002), May 3, 1956.

II II II II U II l.il.III II II LI U II II II II IC 11 IF,

55

622.

623.

624.

625.

626.

627.

628.

629.

630.

631.

632.

Rowley, R. W. An Experimental Investigation of Uncooled Thrust Chamber

Materials for Use in Storable Liquid Propellant Rocket Engines. Jet

Propulsion Lab., California Inst. of Techn__oo!ogy, RePort

No. NASA-TR-32-_61-'(c_-x_fract-Nol NAS 7-I00), Feb. 15, 1964.

Rudinger, George. Dynamics of Gas-Partlcle Mixtures With Finite Par-

ticle Volume. Cornell Aeronautical Lab., Buffalo, N.Y., Rept.

No. CAL-91-P, Office of Naval Res.; Project Squid, December 1964.

Some Properties of Shock Relaxation in Gas Flows Carrying Small

Particles. Cornell Aeronautical Lab., Buffalo, N.Y., Rept.

No. TR-CAL-87-P; Office of Naval Res.; Project Squid (NOmr-3623-(00),NR-098-038), July 1963.

Rudinger, George, and Angela Chang. Analysis of Nonsteady Two-Phase

Flow. Cornell Aeronautical Lab., Buffalo, N.Y., Tech. Rept.

No. CAL-88-P; Office of Naval Res.; Project Squid-(NOmr-3623-(00),

NR-098-038), June 1964.

Rupe, Jack H. A Correlation Between the Dynamic Properties of a Pair of

Impinging Streams and the Uniformity of Mixture-Ratlo Distribution in

the Resulting Spray. Jet Propulsion Lab., California Inst. of Tech-

nology, Progress Rept. No. 20-209; U.S. Army, Ordnance Dept. (contract

No. I_-04-495-Ord-18), Mar. 28, 1956.

On the Dynamic Characteristics of Free Liquid Jets and a Partial

Correlation With Orifice Geometry. Jet Propulsion Lab., California

Inst. of Technolggyi_Rep?KtN_po_l_kSA.TR.32,207 (contract

No. NAS 7-100), Jan. 15, 1962.

A Dynamlc-Head Probe for Evaluating the Properties of Free

Liquid Jets. Jet Propulsion Lab., California Inst. of Technology,

Progress Rept. No. 20-299; U.S. Army, May 23, 1956, 15 pp.

Rupe, Jack H., and David D. Evans. Designing for Compatibility in High-

Performance LP Engine ss_ _Astronautlcs and Aeronautics, v. 3, No. 6,

June 1965, pp. 68-74.

Rybanin, S. S. A Unldlmenslonal Mode] for Detonation in Heterogeneous

Systems. (Translation) Doklady Akademll Nauk SSSR, v. 168, No. 4,

June 1966, pp. 857-859.

Saad, Michel A., and Samuel R. Goldwasser. Role of Pressure in Sponta-

neous Ignition. AIAA J., v. 7, No. 8, August 1969, pp. 1574-1592.

Sabanejeff, A. Some Inorganic Hydrazine Salts and the Preparation of

Hydrazoic Acid. Zeltschrift F_r Anorganische Chemie, v. 20, No. I,

March 1899, pp. 21-29.

56

633.

634.

635.

636.

637.

638.

639.

640.

641.

642.

643.

644.

Sabersky, Rolf H. Effect of Wave Propagation in Feed Lines on Low-

Frequency Rocket Instability. Jet Propulsion, v. 24, No. 3, 1954,

pp. 172-174.

Saier, E. L., and A. Pozefsky. Quantitative Determination of Nitric

Oxide and Nitrous Oxide by Infrared Absorption. Analytical Chemistry,

v. 26, No. 6, June 1954, pp. 1079-1080.

Salooja, K. C. Influence of Surface-to-Volume Ratio of Quartz Reaction

Vessels on Preflame and Ignition Characteristics of Hydrocarbons. Com-

bustion and Flame, v. 8, September 1964, pp. 203-213.

Saltzman, Bernard E. Preparation and Analysis of Calibrated Low Concen-

trations of Sixteen Toxic Gases. Analytical Chem., v. 33, No. 8, July

1961, pp. II00-IIIi.

Saltzman, Bernard E., and Arthur F. Wartburg, Jr. Precision Flow Dilu-

tion System for Standard Low Concentrations of Nitrogen Dioxide. Ana-

lytical Chem., v. 37, No. I0, September 1965, pp. 1261-1264.

Salzman, Jack A., and William J. Masi_ca. E_er_entallnvestigati0n of

Liquld-Pr6peliant Reorientatlon. Report No. NASA TN D-3789, Lewis

Res. Center, Cleveland, Ohio, January I/)67, 20 pp.

Sarner , Stanlez. Mgn__thyl Hydrazine (MMH).-Astronautics (Astro-

nautics Data Sheet--Propellants), July l_60,--p.-f-66.

Sate, Takashl, Ry_ichl Matsumoto, and Akira Yamamoto. Combustion Oscil-

lation in Oil Mist Firing. Japan. Soc. of Mech. Eng., Bull., v. 6,

No. 2, February 1963, pp. 69-77.

Sawyer, Robert F. The Homogeneous Gas Phase Kinetics of Reactions in

the Hydrazine-Nitrosen Tetroxlde Propellant System. Princeton Univ.,

New Jersey, Tech. Rept. No. TR-761, Apr. 7, 1966, 315 p_. Report

No. AFOSR 66-0855, U.S.A.F. _contract-No. AF(638)-i268(9711)).

Sawyer, R. F., and I. Glassman. Gas-Phase Reaction of Hydrazine With

Nitrogen Dioxide, Nitric Oxide, and Oxygen. llth Symp. (International)

on Combustion, at the Univ. of Callfornla, Berkeley, Calif., Aug. 14-20,

1966. Pub. by the Combustion Inst., 1967_-pp. 86_-8-6_

Reaction Kinetics of the Hydrazine-Nitrogen Tetroxide Propellant

System. 2nd Combustion Conf., Interasency Chem. Rocket Propulsion

Group, at Aerospace Corp., Los Angeles, California, Nov. 1-5, 1965;

CPIA Pub. No. 105, v. I, May 1966, pp. 247-250. Air Force Office of

Sci. Res., USAF(contract No. 49(638)-1268).

Schaeffer, J. I. Rocket Exhaust Sampling System for Two Phase Exhaust

Flow Systems. Thiokol Chem. Corp., Reaction Motors Div., Denville,

N.J., Rept. RMD-2103-¥, U.S.A.F. (contract AF 04(611)-6351), 1963.

111 U_U U UU U U L{ U ][ ][ ],{ ],[ E E [

57

645.

646,

647.

648.

649.

650.

651.

652.

653.

654.

Schalla, Rose L., and Edward A. Fletcher.

ous Amines With White Fuming Nitric Acid.

v. 29, January 1959, pp. 33-39.

The Ignition Behavior of Vari-

A.R.S.J. (Jet Propulsion),

Schmldt, Jacob M. An Experimental Study of the Behavior of Liquid

Streams Injected Into a Low-Pressure Chamber. Power Plant Lab., Air

Materiel Command (contract No. W-535-ac-20260); Power Plant Lab., Air

Materiel Command (contract No. W33-038-ac-4320); ORDCIT Project,

Ordnance Dept. (contract No. W-04-200-ORD-455); Jet Propulsion Lab.,

Progress Rept. No. 4-94, California Inst. of Technology, Pasadena,

Calif, Apr. 22, 1949.

Schuyler, Fred L. Combustion Instability: Liquid Stream and Droplet

Behavior. Part I. Experimental and Theoretical Analysis of Evapo-

rating Droplets. Wrlght-Patterson Air Force Base, Wright Air Devel.

Center, Aeronautical Res. Lab. (ARDC) (contract No. AF 33(616)-5163),

September 1960, 52 pp. Report No. WADC-TR-59-720.

Schweitzer, P. H. Mechanism of Disintegration of Liquid Jets. J. of

Applied Phys., v. 8, August 1937, pp. 513-521.

Scott, Frank E., John J. Burns, and Bernard Lewis. Explosive Properties

of Hydrazlne. BuMines Rept. of Inv. 4460, May 1949.

Seagrave, R. C., H. H. Reamer, and B. H. Sage. Oxides of Nitrogen in

Combustion: Oscillatory Combustion at Elevated Pressure. Combustion

and Flame, v. 9, March 1965, pp. 7-18.

Seamans, T. F., and B. E. Dawson. Hypergolic Ignition at Reduced Pres-

sures. Thiokol Chem. Corp., Reaction Motors Dlv., Rept.

No. RMD-5809-F, June 1967, 126 pp. Air Force Rocket Propulsion Lab.,

Edwards Air Force Base, Calif.(contract No. AF 04(611)-I1630).

Report No. AFRPL-TR-67-129.

Seamans, T. F., M. Vanpee, and V. D. Agosta. A Fundamental Model of

Hypergollc Ignition in Space-Amblent Engines. AIAA J., v. 5, No. 9,

September 1967, pp. 1616-1624.

Seamans, T. F., and P. C. Wager. Effects of Additives on Ignition Delay

and Chamber Pressurization of Space-Ambient Engines. Thlokol Chem.

Corp., Reaction Motors Div., Tech. Stmmnary Rept. No. RMD-5533-51,

October 1968, 65 pp. Report No. AFRPL-TR-68-194, Air Force Rocket

Propulsion Lab., Edwards Air Force Bsse, Calif. (contract

No. FO 4611-68-c-0051).

Effects of Additives on Ignition Delay and Chamber Pressuriza-

tion of Space-Amblent Engines. Thlokol Chem. Corp., Reaction Ms=ors

Div., Rept. No. RMD-5533-F, July 1969, 166 pp. Report

No. AFRPL-TR-69-68, Air Force Rocket Propulsion Lab., Edwards Air

Force Base, Calif. (contract No. FO 4611-68-C-0051).

L! ll LI II II II 1] 1[ U U l! II kl 11 U I,:

58

655.

656.

657.

658.

659.

660.

661.

662.

663.

664.

665.

Seel, Fritz, Walter Birnkraut, and Erhard Lange. Zur Frage der Isomericdes Distickstofftetroxides: Kinetic der Umsetzung yon Stlckstoffioxid

mit Stickstoffwasserstoffs_ure in der Gasphase (The Isomerism of

Dinitrogen Tetroxide: Kinetics of the Reaction of Nitrogen Dioxide

With Hydrazoic Acid). Chemisch Berichte, v. 94, No. 6, June 1961,

pp. 1436-1442.

Seel, F., R. WSlfle, and G. Zwarg. Zur Kinetic der Umstezung von

Salpetriger Saute mit Stickstoffwasserstoffs_ure (Kinetics of the

Decomposition of Nitrous Acid With Hydrazolc Acid). Zeitschrift fur

Naturforschung, v. 13b, 1958, pp. 136-137.

Sennett, Robert E. Effectiveness of Multisheet Structures for Meteoroid

Impact Protection. AIAA J., v. 6, No. 5, May 1968, pp. 942-944.

Serewicz, A.,and W. Albert Noyes, Jr. The Photolysis of Ammonia in the

Presence of Nitric Oxide. J. of Phys, Chem., v. 63, 1959, pp. 843-845.

Shaffer, Francis B. Probability of Meteoroidal Penetration. AIAA J.,

v. 2, No. 4, April 1964, pp. 738-742.

Shapiro, N. Z. A Generalized Technique for Eliminating Species in Com-

plex Chemical Equilibrium Calculations. Rand Corp., Rept.

No. RM-4205-PR, U.S. Air Force (contract No. AF 49(638)-700), Septem-

ber 1964.

Shaulov, Yu. Kh., and M. O. Lerner. Combustion in Liquid Propellant

Rocket Motors. Wright-Patterson Air Force Base, Foreign Tech. Div.,

Tech. Transl. FTD-MT-64-272, July 31, 1964, 235 PP. Moscow, 1961

(orig. pub.).

Shaw, J. W. 50-Pound Thrust Attitude-Control Motors. U.S. Naval Ord-

nance Test Station, Propulsion Devel. Dept., NOTS-TP-3206, NAVWEPS-

8118, May 1963.

Shevelyuk, M. I. Teoreticheskiye Osnovy Proyektirovaniya Zhidkostnykh

Raketnykh Dvigateley (Theoretical Bases for the Design of Liquid-

Fueled Rocket Engines). Gosudarsrvennoye Nauchno-Tekhnicheskoye

Izdatel'stvo Oboronglz, Moskva--1960, MCL-1358/I+2, pp. 1-684. Uned-

ited rough draft transl, prepared by Transl. Services Branch, Foreign

Tech. Div., Wright-Patterson AFB, Ohio, Mar. 7, 1962, pp. 1-952.

ASTIA Cat. No. AD 273-887.

Shidlovskii, A. A., V. I. Semishin, and V. I. Simutin. Thermal Decompo-

sition and Combustion of Hydrazine Nitrate. Zhurnal Prikladnoy Khimii,

v. 33, No. 6 (TPI. Z63, v. 33), 1960, pp. 1411-1413. Prepared by Sci.

and Tech. Section; Air Information Div., ASTIA Cat. No. AD-245000,AID-60-42.

Siefker, Joseph R., and E. D. Coon. A Spectrophotometrlc Study of the

Dissociation of Dinitrogen Tetroxide. PToc. of North Dakota Acad. of

Sci., v. XI, 1957, 6 pp.

59

666.

667.

668.

669.

670.

671.

672.

673.

674.

675.

Simmons, John A., and Ralph D. Gift. Phenomena Associated With the

Exposure, Leakage, and Discharge of Propellants Into a Vacuum. Paper

pres. at the 56th Air Force-Industry Conf., at Los Angeles, Calif.,

Feb. 24-26, 1965, 16 pp. Atlantic Res. Corp., Advanced Tech. Div.,

Alexandria, Va. NASA (contract No. NAS8-II044), Feb. 8, 1965.

Simmons, J. A., R. D. Gift, J. M. Spurlock, and R. F. Fletcher. Reac-

tions and Expansion of Hypergolic Propellants in a Vacuum. AIAA J.,

v. 6, No. 5, May 1968, pp. 887-893. NASA (contract NAS 9-6105).

Simoneit, B. R., A. L. Burlingame, D. A. Flory, and I. D. Smith. Apollo

Lunar Module Engine Exhaust Products. Science, v. 166, No. 3906,

November 1969, pp. 733-738.

Sirlgnano, William A. A Theoretical Study of Non-Linear Combustion

Instability: Longitudinal Mode. Princeton Univ., Dept. of Aerospace

and Mech. Sci., Rept. No. TR-677, March 1964, 248 pp. NASA (grant

No. NsG-99-60).

Sirignano, W. A., and W. C. Strahle. A New Concept in Rocket Engine

Baffles. AIAA J., v. 3, No. 5, May 1965, pp. 954-956.

Skinner, G. B., W. H. Hedley, and A. D. Snyder. Mechanism and Chemical

Inhibition of the Hydrazine-Nitrogen Tetroxide Reaction. Monsanto

Res. Corp., Dayton, Ohio; U.S. Air Force, Aeronautical Systems Div.,

ASD-TDR-62-1041, Flight Accessories Lab., Wrlght,Patterson Air Force

Base, Ohio (contracts AF 33(616)-7757 and AF 33(657)-7617), December

1962, 29 pp.

Smith, A. J., Jr., and F. H. Reardon. Development of a Varlable-Length

Chamber for Liquid Rocket Combustion Research. Aerojet-General Corp.,

Rept. 212/SA3-F, v. 3; BSD-TDR-64-137 Product Engineering Final Rept.,

v. 3, October 1964, 94 pp. U.S. Air Force Systems Command (contract

No. AF 04(694)-212/SA 19, item 4).

Smith, L. C., and S. R. Walton. Miscellaneous Physical Testing of

Explosives. U.S. Naval Ordnance Lab., White Oak, Silver Spring, Md.,

Memo. 10381, Sept. 21, 1949, 7 pp.

Sokolowski, Daniel E., Dayi__dW_Vincent, and E. William Conrad. Charac-

terization of l>ressure_Perturbatlonsln_uced in a Rocket Combustor b_y _

a-_a--c_i-_--'-G-un'_Re_ No. NASA-TN D-§214_ Lewis Res. Center,

Clevela ,Ohio, ....

Sommer, Fritz. Studlen_er das Hydrazln und seine anorganischen

Derlvate. I. Uber Hydrazinnitrite und ihre Zersetzungsprodukte

(Studies on Hydrazlne and Its Inorganic Derivatives. I. Hydrazine

Nitrite and Its Decompositlon Products). Zeltschrlft f_r Anorganische

Chemle, v. 83, No. 2, Oct. 2, 1913, pp. 119-137.

60

676.

677.

678.

679.

680.

681.

682.

683.

684.

685.

686.

Sommer, Fritz. Studien _%er das Hydrazln und seine anorganischen

Derivate. II. Die Monotrople des Hydrazinnitrats _it einigen

Bemerkungen _ber die Oxydatlon des Hydrazins). (Studies on Hydrazine

and Its Inorganic Derivatives. II. Monotropism of Hydrazlne Nitrate).

Zeitschrift f_r Anorganlsche Chemle, v. 86, No. I, Feb. 27, 1914,

pp. 71-86.

Somogyi, Dezso, and Charles E. Feller. Liquid-Phase Heat-Release Rates

of the Systems Hydrazine-Nitric Acid and Unsymmetrical Dimethylhydra-

zine-Nitric Acid. Report No. NASA-TN D-469, Lewis Res. Center,

Cleveland, Ohio, September 1960, 16 pp.

Mixture Ratio Distribution in the Drops of Spray Produced by

Impinging Liquid Streams. A.R.S.J., v. 30, February 1960,

pp. 185-187.

Sorter, J. G., and R. M. Clayton. Monitoring the Combustion Process in

Large Engines. J. Spacecraft, v. 4, No. 5, May 1967, pp. 702-703.

Spadaccini, Louis, J. Pressure Gradients in a Variable Area Liquid-

Propellant Rocket Motor. J. of Spacecraft and Rockets, v. 3, No. 7,

July 1966, pp. 1128-1130.

Spakowski, Adolph E. The Thermal Stability of Unsy_netrical Dimethyl-

hydrazine. NASAMemo. 12-13-58E, Lewis Res. Center, Cleveland, Ohio

December 1958, 12 pp.

Spengler, G. Correlation Between Chemical Composition and Ignition

Delay of Hypergolic Rocket Fuels. Deutsche Versuchsaustalt fur Luft-

und Raumphurt, Munich, W. Germany, Inst. fur Flugtrieb-und

Schmierstoffe, October 1963, 16 pp.

Spengler, G., and J. Bauer. Uber den Zundverz_g Hypergoler Raketentreib-

stoffe (On the Ignition Delay of Hyper8olic Rocket Propellants).

Brennstoff-Chemie, v. 46, No. 4, April 1965, pp. 117-124.

Uber Hypergole Raketentrelbstoffe das Zundverhalten fl_ssiger.

Treibstoffkombinationen unter vermlndertem Brennkammerdruck (On Hyper-

gole Rocket Propellants. Ignition State of Fluid Propellant Combina-

tions Under Reduced Pressure of Combustion Chamber). Brennstoff-

Chemic, v. 47, No. 4, 1966, pp. 110-114.

Spengler, G., A. H. Lepie, and J. Bauer. Measurement of Ignition Delays

of Hypergolic Liquid Rocket Propellant. Paper No. 64-12, pres. at the

1964 Spring Meeting, Western States Section, The Combustion Inst.,

Stanford Univ., April 1964, 22 pp.

Sprague, Robert W. Solubility of Oxygen in White and Red Fuming Nitric

Acids. Industrial and Eng. Chem., v. 47, No. II, November 1955,pp. 2396-2398.

61

687.

688.

689.

690.

691.

692.

693.

694.

695.

696.

697.

698.

Sprague, Robert W., --d Ethel Kaufman. Densities of Ternary System

Nitric Acld-Dinitrogen Tetroxide-Water. Industrial and Eng. Chem.,

v. 47, No. 3, March 1955, pp. 458-460.

Spring, T. R., and D. J. Hatz. Propellant Hazards Evaluation. Rocket-

dyne, a div. of North American Aviation, Inc., Canoga Park, Calif.,

pp. 387-396. U.S. Air Force (contract No. AF 33(616)-6939).

Starrett, P. S., and P. F. Halfpenny. Impulse Bit Measurement for Small

Pulsed Rocket Motors. AIAA J., v. I, July 1963, pp. 1679-1681.

Stedman, G. Mechanism of the Azide-Nitrlte Reaction, Parts I and II.

J. of the Chem. Soc. (London), 1959, pp. 2943-2954.

Stengel, Leonard A., and Emory E. Toops, Jr. Stable Propellants. U.S.

Pat. 3,061,489, assigned to Commercial Solvents Corp., Terre Haute,

Ind., Oct. 30, 1962.

Stepka, Francis S., and C. Robert Morse. Preliminary Investigation of

Catastrophic Fracture of Liquid,Filled Tanks_ Impac_edby High-Velocity

Particles. Report No. NASA TN D-1537, Lewis Res. Center, Cleveland,

Ohio, May 1963, 28 pp.

Stevens, Mario R., H. Dwight Fisher, Harold G. Weiss, and Bernard P.

Breen. Effect of Additives on the Ignition Delay Time of Hypergolic

Propellants. Dynamic Sci., a div. of Marshall Industries, Monrovia,

Calif., Final Rept. (Draft), Mar. 31, 1967, 43 pp. NASA/Pasaden_ Jet

Propulsion Lab., California Inst. of Technology, Calif. (contract

No. NAS 7-438).

Stief, L. J., and V. J. Deearlo. Vacuum-Ultraviolet Photochemistry.

VIII. Photolysis of Hydrazine-lSN in the Presence of 14NO at 1470 _.

J, of Chem. Phys., v. 49, No. I, July I, 1968, pp. 100-105.

Stoll_, R. Die titrimetrische Bestimmung von Hydrazine und die

Verwendung von Hydrazinsulfat zur Titerstellung der Jodl_sung (The

Titrimetric Determination of Hydrazine and the Application of Hydra-

zinc Sulfate in the Standardization of Iodine Solutions). J. fur

Praktische Chemle, v. 66, 1902, pp. 332-338.

Strahle, Warren C. A Theoretical Study of Unsteady Droplet Burning:

Transients and Periodic Solutions. Princeton Univ., Guggenhelm Lab.

for the Aerospace Propulsion Sol., Dept. of Aeronautical Eng., Rept.

No. AEL-671, NASA (grant No. NsG-99-60), January 1964.

A Transient Problem on the Evaporation of a Reactive Fuel. Com-

bustion Sci. and Tech., v. I, July 1969, pp. 25-33.

Strahle, Warren C., and L. Crocco. Analytical Investigation of Several

Mechanisms of Combustion Instability. Princeton Univ., Princeton,

N.J., NASA (grant No. NsG-99-60), Nov. 15, 1963, 25 pp. Report

No. NASA-CR-52632.

%\

II II II II II tl IJ kl U U II I/ ti II II II II I,; L" Ii

62

699.

700.

701.

702.

703.

704.

705.

706.

707.

708.

Strauss, W. A., J. W. Pllckebaum, and R. Edse. Combustion Phenomena as

a Function of Pressure. Ohio State Univ., Dept. of Aeronautical Eng.,

Aeronautical Res. Lab., Rept. No. ARL-61, September 1961.

Suarez-Alfonso, E., A. E. Chambers, and D. J. Hatz. Hydrazine Handling

Manual. Rocketdyne, a div. of North American Aviation, Inc., Canoga

Park, Calif., Rept. No. 3134, September 1961, 57 pp. Report

No. AF/SSD-TR--6I-?,--Air Force, Spade-_ystem_D_-_.,Edw_ds Air Force

Base, Calif. (comtract No. AF 33(616)-6939).

Mechanical System Design-Criteria Manual for Hydrazine. Rocket-

dyne, a div. of North American Aviation, Inc., Canoga Park, Calif.,

Rept. No. 3130, September 1961, 79 pp. Report No. AF/SSD-TR-61-6,

Air Force, Space Systems Div., Edwards Air Force Base, Calif. (con-

tract No. _KF 33(616)-6939).

Mechanical System Design-Criteria Manual for Nitrogen Tetroxide.

Rocketdyne, a dlv. of North American Aviation, Inc., Canoga Park,

Calif., Rept. No. 3131, September 1961, 83 pp. Report

No. AF/SSD_TR-61L_,-A-irFor--_,-Space-Systeam-Div., Edwards Air Force

Base, Callf. (contract No. AF 33(616)-6939).

Nitrogen Tetroxide Handling Manual. Rocketdyne, a div. of North

American Aviation, Inc., C_a_nQEa Parkj C_alif., Rept. No. 3135, September

1961, 58 pp. Report No, AF/SSD-TR-61-8, Air Force, Space Systems Div.,

Edwards Air Force Base, Calif. (contract No. AF 33(616)-6939).

Summerfield, Martin. The Theory of Unstable Combustion in Liquid Pro-

pellant Rocket Systems. J. of the American Rocket Soc., v. 21, No. 5,

September 1957, pp. 108-114.

Svehla, Roger A., and Richard S. Brokaw. Thermodynamic and Transport

Properties for the NaO_ = 2NO _ = 2NO +Os System. ReportNo. NASA-TN D-3227, Lewis Res. Center, Cievelan_,_Oh-lo, March 1966.

Svirldov, Yu. B. The Nature of Ignition of Atomized Fuels From the Dif-

fusion and Kinetics Polnt of View. An SSSR Lavoratoriya Dvlgateley

Trudy (A_ademy of Scl. of the USSR; Reports of the Laboratory for

Engines (or Motors)); Air Force Systems Command, Foreign Tech. Div.,

Wright-Pat=erson Air Force Base, Rept. No. FTD-MT-24-84-68, May 3,

1968 (Transl. date), 24 pp.

Szuch, John R., and Leon M. Wenzel. Experimental Verification of a

Double Dead-Time Model DescrlbingChugglng in Liquid Bipropellant

Rocket Eng_ines. Report No. NASA-TN D-4564, Lewis Res. Center,

Cleveland, Ohio, May 1968.

Tait, C. W., J. A. Happe, R. W. Sprague, and H. F. Cordes. Kinetics of

Thermal Decomposition of Liquid Nitric Acid. J. of the American Chem.

Soc., v. 78, 1956, pp. 2670-2673.

U II II II U ]J I,I U U U U II II II II II £ £

63

709.

710.

711.

712.

713.

714.

715.

716.

717.

718.

719.

720.

721.

Takimoto, H. H., and G. C. Denault. Combustion Residues From NeO_-MMH

Motors. The Aerospace Corp., E1 Segundo, Calif., Aerospace Rept.

No. TR-0066(5210-I0)-I, September 1969, 22 pp. U.S. Air Force, Space

and Missile Systems Organ., Air Force Systems Conxnand, Los Angeles Air

Force Station, Los Angeles, Calif., Rept. No. SAMSO-TR-69-373.

Tallman, Charles R. Transducer Frequency Response Evaluation for Rocket

Instability Research. A.R.S.J., v. 29, 1959, pp. 119-122.

Tarifa, Carlos Sanchez. Combustion of Solid and Liquid Propellants and

Flame Theory. Instituto Nacional de Teknica Aeronautica, Esteban,

Terradas, AFOSR, Rept. No. OSR/EOAR-TR (contract No. AF 61(052)-221),

May I, 1962.

Tarifa, C. S_nchez, and P. P_rez del Notario. Combustion of Monopropel-

lant Droplets: Theoretical Results. Instituto Nacional de Teknica

Aeronautica, Bsteban, Terradas (contract No. AF 61(514)-997), Dec. 15,

1958. Report No. AFOSR-TN-59-463.

. A Theoretical Investigation on the Combustion of Liquid Bipro-

pellant Droplets. Instituto Nacional de Teknica Aeronautica, Esteban,

Terradas (contract No. AF 61(052)-221), Apr. ii, 1960. Report

No. AFOSR-TN-59-975.

Tarifa, C. Sanchez, P. Perez del Notario, and F. Garcia Moreno. Combus-

tion of Liquid Monopropellants and Bipropellants in Droplets. 8th

Symp. (International) on Combustion, Paper 109, at the California

Inst. of Technology, Pasadena, Calif., Aug. 28-Sept. 3, 1960,

pp. 1035-1056. Pub. by Williams and Wilkins Company, Baltimore, 1962.

Taylor, J. Detonation in Condensed Explosives. Oxford at the Clarendon

Press, 1952.

Taylor, J., and J. H. Cook. Improved Operation of the Ballistic Mortar

for Determining the 'Rower" of High Explosives. J. of Sci. Instru-

ments and Phys. in Ind., v. 26, No. 8, August 1959, pp. 266-268.

Taylor, W., and G. Morris. The Absolute Measurement of the Available

Energy of High Explosives by the Ballistic Mortar. Trans. Faraday

Soc., v. 28, 1932, pp. 545-558.

Thomas_ J. H. Oxidation Reactions Involving Nitrogen Dioxide. Oxida-

tion and Combustion Reviews, v. I, 1965, pp. 137-168.

Thomas, P. H. A Comparison of Some Hot Spot Theories. Combustion and

Flame, v. 9, December 1965, pp. 369-372.

Thomson, William T. An Approximate Theory of Armor Penetration. J. of

Applied Phys., v. 26, January 1955, pp. 80-82.

Note on '_n Approximate Theory of Armor Penetration." J. of

Applied Phys., v. 26, 1955, pp. 919-920.

64

722.

723.

724.

725.

726.

727.

728.

729.

730.

731.

732.

733.

734.

Tiner, N. A., L. E. Bell, and S. M. Toy. A NewApproach to Impact Sensi-tivity Testing in Liquid Propellant Systems. Paper No. 5027, pres. atthe CryogenicTech. 1968 Session of WESTECConf., Los Angeles, Calif.March 1968, 15 pp.

Tkachenko, E.A. DynamicScience Computer Program for Hypergolic Pro-pellant Space Starts. DynamicSci., a div. of Marshall Industries,Tech. Brief No. B-48, January 1968, 5 pp.

Tobey, Aubrey C. Combustion Instability Studies. 1964 Spring Meeting,Western States Section, The Combustion Inst., Stanford Univ., PaperNo. WSS/CI64-10, April 1964, 45 pp. U.S.A.F. (contractNo. AF 49(638)-1120).

Tomazic, William A., and George R. Kinney. Experimental Performance ofthe Mixed-Oxides-of-Nitrogen-Ammonla Propellant Combination With Sev-eral Injection Methods in a I000 PoundThrust Rocket Engine. ReportNo. NACA-RM-E55A07,Mar. 4, 1955-_ ....

Toong, Tau-Yi, Richard F. Salant, John M. Stopford, and Griffin Y.Anderson. Mechanismsof Combustion Instability. Massachusetts Inst.of Tech., U.S. Air Force, 1964.

Torda, T. P., and B. R. Patel. Analytical and Experimental Investiga-tions of Oscillations in Rocket Motor Baffle Cavities. Illinois Inst.of Tech., Dept. of Mech. En_. , Chicago, III., Final Summary Rept.,

May 1968, 14 pp. Report. No. AFOSR-68-i369, U.S_ Air Force (contract

No. AF AFOSR-I081-66, Project No. 9711).

Torda, T. Paul, and Leo A. Schmidt. One Dimensional Unsteady Aero-

Thermochem/cal Analysis of Combustion Instability in Liquid Rocket

Engines. Pyrodynamics, v. I, 1964, pp. 89-111.

Trent, C. H., and M. J. Zucrow. The Hypergolic Reaction of Dicyclopen-

tadiene With White Fuming Nitric Acid. J. of the American Rocket Soc.,

v. 21, No. 5, September 1957, pp. 129-131.

Trotman-Dickenson, A. F. Gas Kinetics. Pub. by Butterworths Sci. Pub-

lications, London, 1955.

Tsien, H. S. Servo-Stabillzation of Combustion in Rocket Motors.

A.R.S.J., v. 22, 1952, pp. 256-262, 268.

Turney, T. A., and G. A. Wright. Nitrous Acid and Nitrosation. Chem.

Reviews, v. 59, January-June 1959, pp. 497-513.

Tyler, E. Instability of Liquid Jets. Phil. Mag. S.7., v. 16, No. 105,Suppl., August 1933, pp. 504-518.

Udelson, D. G. Geometrical Considerations in the Burning of Liquid

Drops. Combustion and Flame, v. 6, June 1962, pp. 93-102.

65

735.

736.

737.

738.

739.

740.

741.

742.

743.

744.

Underwood, A. L., Michael W. Miller, and Lyman H. Howe, III. Infrared

Spectrophotometry of Aqueous Nitrate, Nitrite, and Sulfate Solutions.

Anal. Chlm. Acta, v. 29, 1963, pp. 79-81.

Upper, Charles E., and Stanley Lehrer. Program To Study and Resolve

Rocket Engine Installation Problems Related to Maneuvering Satellite

Vehicles._Astrosystems Internatlona_ Inc., Fairfield, N.J., Tech.

Rept. No. 63080F; E_or6-No_F-KPLLTR2_5-4_ ,-Air Force Rocket Propul-

sion lab., Res.and _h. Biv., Air Eorce Systems Co_nand, Edwards AFB,

Calif. (contract _l_T._(61Fl")-_9565)_-Fe_-f'4/ [965_

Urry, W. H., A. L. Olsen, E. M. Bens, H. W. Kruse, C. Ikoku, and

Z. Galbel. Autooxldatlon of l,l-Dimethylhydrazine. U.S. Naval Ord-

nance Test Station, China Lake, Calif. (an activity of the Bureau of

Naval Weapons), NOTS Tech. Pub. 3903, NAVWEPS Rept. 8798, September

1965, 38 pp.

Urry, W. H., A. L. Olsen, and H. W. Kruse. Use of Infrared Spectroscopy

in Studies of the Autooxidation of Methylhydrazines. Paper No. 307,

pres. at the Pacific Conf. on Chemistry and Spectroscopy, Anaheim,

Calif., Oct. 6-10, 1969.

Van Dolah, Robert W., Michael G. Zabetakis, David S. Burgess, and

George S. Scott. Revlew of Fire and Explosion Hazards of Flight

Vehicle Combustibles. BuMines, Explosives Res. Center, Pittsburgh,

Pa., Inf. Circ. 8137, 1963, 80 pp. Flight Accessories Lab., Aero-

nautical Systems Div., Air Force System, s Coumnand, Wright-Patterson

Air Force Base (contract No. DO (33-616)60-8).

Vango, Stephen P., and John B. Krasinsky. Density, Vapor Pressure and

Viscosity of Solutions of Hydrazine Mononitrate in Hydrazine. Jet


Tech. Memo. No. 33-103, Oct. 15, 1962, 12 pp. NASA (contract

No. NAS 7-I00).

Hydrazine Nitrate in Hydrazine; Supplemental Physical Data.


Tech. Memo. No. 33-122, Mar. 24, 1963, 12 pp. NASA (contract

No. NAS 7-i00).

Jet

Van Tiggelen, P. J. oI,__he Minimal Initial Size of an Explosive Reac-

tion Center. Combustion Scl. and Tech., v. I, 1969, pp. 225-232.

Villemarette, R. J., J. W. Akerman, N. H. Chaffee, B. J. Rosenbaum,

W. D. Taliaferro, and A. K. Watkins. Apollo AFRM 001 Service Module

Reaction Control System Panel B Plus Yaw Engine Failure Analysis.

NASA Manned SpacecraftCenter, Rept. No. MSC-IN-65-EPI7, November 1965.

Vincent, David W., Daniel E. Sokolowski, and Harry E. Bloomer. Screech

Suppression Technique £ for Rock9 _ Cg_ustors Using Earth-Storable

Propellants. Report No. RASA-_-X-1595, Lewis Res. Center, Cleveland,

Ohio, June 1968_-37-pp. .............

66

745.

746.

747.

748.

749.

750.

751.

752.

753.

754.

755.

Vitali, R., K. R. Becker, and R. W. Watson. Perforation of Finite Tar-

gets by High Velocity Projectiles. Proc. 5th Syrup. on Hypervelocity

Impact, at Denver, Colo., v. I, part 2, Oct. 30-Nov. I, 1961. U.S.

Army, Navy, and Air Force (contract No. Nonr-(G)-0020-62(X)), April

1962 (pub. date), Pp. 593-610.

Waesche, R. H. Woodward. Comments on '_ Ballistic Bomb Method for Deter-

mining the Experimental Performance of Rocket Propellants." A.R.S.J.,

v. 29, May 1959, pp. 375-376.

Wasko, RobertA. Reaction of Hydrazine and Nitrogen Tetroxide in a Low-

Pressure Environment. AIAA J., v. I, No. 8, August 1963,

pp. 1919-1920.

Wasserbauer, Joseph F., and William Tabata. Performance of Small

(i00 Ib. Thrust) Rocket M0tors Usin _ Coaxial Injection of Hydrazine and

Nitrogen Tetroxide. Report No. NASA-TN-D-II62, December 1961, 27 pp.

Watson, R. W. The Perforation of Thin Plates by High Velocity Fragments.

Proc. 5th Symp. on Hypervelocity Impact, at Denver, Colo., v. I,

part 2, Oct. 31-Nov. i, 1961, pp. 581-592. U.S. Army, Navy, and Air

Force (contract No. Nonr-(G)-OO20-62(X)), April 1962 (pub. date).

Watson, R. W., K. R. Becker, and F. C. Gibson. Thin Plate Perforation

Studies With Projectiles in the Velocity Range From 2 to 5 KM/Sec.

Proc. 6th Symp. on Hyperveloclty Impact, at Cleveland, Ohio, v. III,

Apr. 30-May 2, 1963, pp. 208-248. U.S. Army, Air Force, and Navy

(contract No. DA-31-124-ARO(D)-I6), August 1963.

Watson, Richard, and Frank Gibson. Je=s From Imploding Bubbles. Nature,

v. 204, December i964, pp. 1296-1298.

Watson, R. W., C. R. Summers, F. C. Gibson, and R. W. Van Dolah. Detona-

tions in Liquid Explosives--The Low-VelocityRegime. Proc. 4th Symp.

(International) on Detonation, at the U.S. Naval Ordnance Lab., White

Oak, Silver Spring, Md., Paper No. ACR-126, Oct. 12-15, 1965,

pp. 117-125. Bureau of Naval Weapons, Dept. of the Navy, (contract

No. 19-6b-8023-WEPS), October 1965.

Wayman, D. H., and R. L. Potter. Detonations in Gaseous Fuming Nitric

Acld-Hydrocarbon Mixtures. Combustion and Flame, v. I, 1957,

pp. 321-329.

Wayne, Lowell G., and Don. M. Yost. Kinetics of the Rapid Gas Phase

Reaction Between NO, NO_ and BQO. J. of Chem. Phys., v. 19, No. I,

January 1951, p. 41.

Webber, William T. Effects of Gas Motion on Heterogeneous Combustion;

Natural Convection, Steady Forced Convection, Standing Acoustic Waves,

and Shock Waves. (FinalSunanaryReport) Rocketdyne, North American

Aviation, Inc.; Report No. WADC-TR-59-50, U.S. Air Force-(c0ntract

No. AF 33(616)-3556), April 1959.

E gIi I1 .1/ 11 Ii 11 1I I.i lg 11 R 1! 11 11 11 II ii g

67

756.

757.

758.

759.

760.

761.

762.

763.

764.

765.

766.

Spray Combustion in the Presence of a Travelling Wave. 8th

Symp. (International) on Combustion, at the California Inst. of Tech-

nology, Pasadena, Calif., Paper No. 121, Aug. 2B-Sept. 3, 1960,

pp. 1129-1140; pub. by Williams and Wilkins Company, Baltimore, Md.,

1962. U.S. Air Force, Aeronautical Res. Lab., Wright Air Devel. Cen-

ter (contract No. AF 33(616)-3556).

Weinberg, F. J., and J. R. Wilson with an Appendix by J. Adler. An

Optical Study of Pre-lgnitlon Heat Release. Proc. of Roy. Soc. of

London, Ser. A, 314, 1970, pp. 175-193.

Weiss, Harold G. A Basic Study of the Nitrogen Tetroxide-Hydrazine

Reaction. Dynamic Sci. Corp., Monrovia, Calif., Rept. No. SN-4500;

Jet Propulsion Lab. (contract No. BE 4-229751), subcontract to NASA

(contract No. NAS 7-100), July 1965.

. Chemical Factors in NmO4-NmH _ Liquid Reactions. Paper

No. WSCI-65-20, pres. at the 1965 Fall Meeting of the Western States

Section of the Combustion Inst., NASA (contract No. NAS 7-100),Oct. 25, 1965.

Effect of Additives on the Ignition Delay Time of Hypergolic

Propellants. Dynamic Sci., a div. of Marshall Industries, Monrovia,

Calif., Quart. Rept. No; 2, Apr. 5-July 4, 1966; NASA (contract

No. NAS 7-438), July 15, 1966.

Weiss, Harold G., Bruce Johnson, H. Dwight Fisher, and Melvin Gerstein.

Modification of the Nydrazlne-Nitrogen Tetroxide Ignition Delay• AIAA

J., v. 2, No. 12, December 1964, pp. 2222-2223.

Weiss, H. G., and E. B. Klusmann. Determination of Miscibility Charac-

teristics of Highly Reactive Liquids. American Chem. Soc. J., v. 84,

Dec. 20, 1962, p. 4993.

Welge, Karl H. Formation of N2 (A3Zu +) and N _D,mP) by Photodissocia-

tion of HN s and NmO and Their Reactions With NO and NmO*i J. of Chem.

Phys., v. 45, No. I, July 1966, p. 166.

Wharton, Walter W., J. W. Connaughton, B. D. Allan, and W. D. Williams.

The Effect of Sound Oscillations on Combustion and Heat Transfer.

U.S. Army, Army Rocket and Guided Missile Agency, Redstone Arsenal,Ala., Rept. No. AR_-TR-IC36R, Dec. 15, 1959.

White, Arvel B. Experimental Investigation of Heat Flux at the Upper

Limit of Nucleate Boiling for Two MixTures of Hydrazine and Unsymmet-

rical Dimethylhydrazi_. Jet Propulsion Lab., California Inst. of

Technology, Rept. No.;JPL_TR-3278; NASA (conTract No. NASW-6),Apr. 6, 1961.

Whitnack, Gerald C., Clifford J. Holford, E. St. Clair Gantz, and

G. B. L. Smith. DeterminaTion of Nitric Oxide and Nitrogen Tetroxide

in Admixture. Anal. Chem., v. 23, March 1951, pp. 464-467.

Ii I/ l/ 1I 1I I1 11 i.I 1I U U 11 11 11 11 il 11 g E lli

68

767.

768.

769.

770.

771.

772.

773.

774.

775.

776.

777.

778.

Whittaker, A. Greenville. Burning-Rate Studies. Part 6. Effect of

Chemical Composition on the Consumption Rate of Various Nitric Acid

Systems. J. of Phys. Chem., v. 62, March 1958, pp. 267-271.

Whittaker, A. Greenville, T. M. Donovan, and H. Williams. Burning Rate

Studies. Part 7. Onset of Turbulent Combustion of Liquids Contained

in Small Tubes. J, of Phys. Chem., v. 62, August 1958, pp. 908-912.

Whittaker, A. G., R. W. Sprague, S. Skolnlk, and G. B. L. Smith. Vapor

Pressures and Freezing Points of the System Nitrogen Tetroxide-Nitric

Oxide. J. of the American Chem. Sot., v. 74, October 1952,

pp. 4794-4797.

Whittaker, A. Greenville, and Harry Williams. Burning-Rate Studies.

Part 5. Effect of Acid Concentration on the Consumption Rate of Vari-

ous Fuels With Nitric Acid. J. of Phys. Chem., v. 61, April 1957,

pp. 388-394.

Whittaker, A. Greenville, Harry Williams, and Penniman M. Rust. Burning

Rate Studies. A Negative Exponent in the Consumption-Rate Equation

for a Liquid System. J. of Chem. Phys., v. 26, No. 3, March 1957,

pp. 717-718.

Wieber, Paul R. Calculated Temperature Histories of Vaporizing Droplets

to the Critical Point. AIAA J., v. I, No. 12, December 1963,

pp. 2764-2770.

Wieber, Paul R., and William R. Mickelsen. Effect of Transverse Acous-

tic Oscillations on the Vaporizatlon of a Liquld-Fuel Droplet. Report

No. NASA-TN-D-287, Lewis Res. Center, Cleveland, Ohio, May 1960, 25 pp.

Wilber, Paul C., Michael A. Merrigan, P. Roy Choudhury, Stephan P. Vango,

and William Lee. On the Spontaneous Ignition of Hypergollc Propellant

Systems at Low Pressures and Temperatures. Paper pres. at the Western

States Combustion Inst. Meeting at Salt Lake City, Utah, Oct. 26-27,

1964, Paper No. WSCI_64-29_ 23 p_. U_,S: Air Force, RPL (contract

No. AF 04(611)-9890), October 1964.

Wilcox, Jerry Dean. Differential Scanning Calorimetry Methods in the

Determination of Thermal Properties of Explosives. GAW/ME/67B-3, Air

Force Inst. of Tech., June 1967, 70 pp.

Wilde, Kenneth A. The Role of HNO in the H_NO Reaction. Combustion and

Flame, v. 13, No. 2, April 1969, pp. 173-180.

Wilhelmi, H. Explosionsdr_cke yon Brenngasen (Explosion Pressures of

Gaseous Fuels). Intern. Z. GaswHrme, v. 13, No. 6 (M/tteilung aus dem

GaswHrme-lnstitut), June 1964, pp. 240-247.

Williams, F.A. Detonations in Dilute Sprays. Progr. Astronaut. Rock-

etry, v. 6, National $ci. Foundation, Res. Grant No. 12146, 1961,

pp. 99-114.

69

779.

780.

781.

782.

783.

784.

785.

786.

787.

788.

789.

__. Progress in Spray-Combustion Analysis. 8th Symp. (International)

on Combustio_at the California Inst. of Technology, Pasadena, Calif.,

Aug. 28-Sept. 3, 1960, Survey Paper No. VI, pp. 50-69. Pub. by

Williams and Wilkens Company, Baltimore, Md., 1962.

• Spray Combustion Theory. Combustion and Flame, v. 3, 1959,pp. 215-228.

Williams, Harry, and A. Greenville Whittaker. Photography in Combustion

Studies. Photographic Sci. and Technique, Section B of PSA J.,

v. 19B, No. 4, November 1953, pp. 161-162.

Willoughby, A. B., and others. NASA/USAF Liquid Propellant Blast

Hazards Program. A series of monthly and quarterly progress repts, by

United Res. Services Corp., Burlingame Res. Center, Burlingame, Calif.

U.S. Air Force Rocket Propulsion Lab. (contract No. AF 04(611)-9558),1965-1966.

Willoughby, A. B., J. Mansfield, T. C. Goodale, and C. Wilton. Summary

of Existing Information Concerning the Explosive Potential of the

Hypergolic Propellant Comb inati0n N pAL/bpTo -50 /o URS Corp.,Burlingame, Calif., Report No. AFRPL-TR-65-27 (contract

No. AF 04(611)-9558), April 1965.

Winning, W. I. H. The Thermal Oxidation of Hydrazine Vapour. J. of theAmerican Chem. Soc._ i954, pp.i 926-931q-

Wise, Henry, Jack Lorell, and Bernard J. Wood. The Effect of Chemical

and Physical Parameters on the Burning Rate of a Liquid Droplet.

5th Symp. (International) on Combustion, at the Univ. of Pittsburgh,

Pittsburgh, Pa., Aug. 30-Sept. 3, 1954, Paper No. 3, pp. 132-141.

Pub. by the Combustion Inst., 1955. Dept. of the Army, Ordnance Corps.

(contract No. DA-04-495-Ord-18), 1955.

Wolfson, Bernard T. The Effect of Additives on the Mechanism of Detona-

tion in Gaseous Systems. Wright-Patterson Air Force Base, Aeronauti-

cal Res. Lab., Rept. No. ARL-63-82, May 1963.

Wood, Bernard J., Henry Wise, and S. Hgn___Inami_ Heterggeneous Combus-tion of Multicomponent Fuels. Report No. NASA-TN-D-206, November 1959.

Wood, Don J., and Robert G. Dorsch. Effect of Propellant-Feed-System

CouplinKand Hydraulic PaKameters on Anal_@is of Chugglng. Report

No. NASA-TN-D-3896, Lewis Res. Center, Cleveland, Ohio, May 1967, 22 pp.

Wood, H. L., and D. A. Charvonia. The Ignition of Fuel Droplets

Descending Through an Oxidizing Atmosphere. Jet Propulsion, v. 24,No. 3, May-June 1954, pp. 162-165.

I/ I/ _i/ IJ 1I U 11 U L; il 11 I1 11 n II II g i;

70

790.

791.

792.

793.

794.

795.

796.

797.

798.

799.

800.

801.

Wrobel, J. R. Effects of Fuel Inlet Temperature Upon the Performance of

a Monopropellant Hydrazine Reaction Chamber. Jet Propulsion Lab.,

California Inst. of Technology, Pasadena, Calif., Tech. Memo.

No. TM-35-132; NASA (contract No. NAS 7-100), July 1963.

Wuerker, R. F., and B. J. Matthews. Producing Holograms of Reacting

Sprays in Liquid PropellantRocket Engines. TRW, Inc., TRW Systems

Group, Power Systems Div., Redondo Beach, Calif., Phase I, Interim

Rept. No. 68.4712.2-017, February 1968, 57 pp. NASA (contract

No. NAS 7-100); Jet Propulsion Lab., California Inst. of Technology,

Pasadena, Calif. (contract No. 952023).

Yang, C. H. Theory of Ignition and Auto-Ignitlon. Combustion and Flame,

v. 6, December 1962, pp. 215-225.

York, H. J. Compatibility of Various Materials of Construction With

Nitrogen Tetroxlde (N_O4). AeroJet General Corp., Res. and Materials

Dept., Rept. No. RM-13, Oct. 22, 1958.

Zeleznik, Frank J., and Sanford Gordon. A General IBM 704 or 7090 Com-

puter Program for Computation of Chemical Equilibrium Compositions,

RQCket Performance, and Chapman-Jouguet Detonations. Report

No. NASA-TN-D-1454, October 1962.

Zinn, Ben T. A Theoretical Study of Nonlinear Combustion Instability in

Liquid-Propellant Rocket Engines. AIAA J., v. 6, No. I0, October 1968,

pp. 1966-1972.

Zinn, John. Initiation of Explosions by Mot Spots. J. of Chem. Phys.,

v. 36, 1962, p. 1949.

Zucrow, M. J., and J. R. Osborn. An Experimental Study of High-

Frequency Combustion Pressure Oscillations. Jet Propulsion, v. 28,

No. i0, October 1958, pp. 654-659.

. Reply to Crocco's Criticism of the Zucrow-Osborn Paper. A.R.S.

J., v. 29, March 1959,.pp_-22T1222.

Zucrow, M. J., J. R. Osborn, and A. C. Pinchak. Luminosity and Pressure

Oscillations Observed With Longitudinal and Transverse Modes of Com-

bustion Instability. A.R.S.J., v. 30, 1960, pp. 758-761.

Zung, L. B., and B. P. Breen. A Basic Study on the Ignition of Hyper-

golic Liquid Propellants. Dynamic Sci., a dlv. of Marshall Industries,

Monrovia, Calif., 2nd Quart. Rept., November 1968, 17 pp. NASA (con-

tract NAS 7-438, Mod. No. 6).

. A Basic Study on the Ignition of Hypergolic Liquid Propellants.

Dynamic Scl., a dlv. of Marshall Industries, Monrovia, Calif., 3d

Quart. Rept., Feb. 20, 1969, 22ppl-NASA(c0ntract No. HAS 7-438, Hod.

No. 6).

Ii If IJ ]IJ U II IJ Ll U II LI ],[ U II II II II L li

71

802.

803.

804.

805.

806.

807.

808.

809.

810.

Zung, Laurence B., B. P. Breen, and Raymond Kushlda. A Basic Study of

Ignition of Hypergollc Liquid Propellants. Paper No. WSCI 68-43,

pres. at the Western States Section/The Combustion Inst., Stanford

Res. Inst., Menlo Park, Calif.; NASA (contract No. NAS 7-438)/JPL,

Oct. 29, 1968.

Zung, L. B., B. R. Lawyer, E. A. Tkachenko, and B. P. Breen. Effect of

Additives on the Ignitlon Delay Time of Hypergolic Propellants.

Dynamic Sci., a div. of Marshall Industries, Ist Quart. Rept., Septem-ber 1967, 12 pp. N_SA (contract No. NAS 7-438, Mod. No. 3).


Propellants. Subject: Analysis of Reaction Products and Ignition

Threshold Study for the System N2Od/Nzl _. Dynamic Sci., a div. of

Marshall Industries, Monrovia, Calif., Quart. Rept., Dec. I, 1967,

21 pp. NASA (contract No. NAS 7-438, Mod. No. 3).


Propellants. Subject: Analysis of Reaction Products and Ignition

Threshold Study for the System N_Od/Nzl _ . Dynamic Sci., a div. of

Marshall Industries, Monrovla, Callf., Quart. Rept., Mar. I, 1968,

38 pp. NASA (contract No. NAS 7-438, Mod. No. 3).

Zung, L. B., E. A. Tkachenko, and B. P. Breen. A Basic Study on the

Ignition of Hypergollc Liquid Propellants. Dynamic Scl., a div. of

Marshall Industrles, Monrovia, Calif , Interim (12 month) Final Rept.

No. SN-80, Mod. 3-F, November 1968. NASA (contract No. NAS 7-438).

Zwick, E. B., and S. J. Minton. An Investigation of Oxidizer Manifold

Explosions (Zots) in the Apollo SM/RCS Engine. Apollo Service Module

Reaction Control Engines. The Marquardt Corp., Van Nuys, Calif.,Rept. No. S-483, February 1966.

Miscellaneous

Format for the Collection of Liquid Propellant Rocket Combustion Insta-

bility Test Data. Prepared by the: Format Committee of the Working

Group on Liquid Propellant Combustion Instability (Interagency Chemi-cal Rocket Propulsion Group (ICRPG)). CPIA Publlcatlon No. 149.

September 1967.

Handbook of Recommended Practices for Measurement of Liquid-Propellant

Rocket Engine Parameters. Prepared by the: Performance Standardiza-

tion Working Group (Interagency Chemical Rocket Propulsion Group).CPIA Publication No. 179_- januaz_ IgE-

Micrometeoroid Satellite (Explorer XlIl) Stalnless-Steel Penetration

Rate Experiment. Prepared by the: Staff of the Lewis Res. Center,

Lewis Res. Center, Cleyeland , Ohio. Report No. NASA-TN-D-1986, LewisRes. Center, October 1963. ---

72

811.

812.

813.

814.

815.

816.

817.

818.

819.

820.

821.

The Penn State Bibliography on Sprays. Second Edition. Prepared by the:

Staff of the Dept. of Eng. Res., The Pennsylvania State Univ. Pub-

lished by: The Texas Company, Refining Dept., Tech. and Res. Div.,

New York. December 1953.

Properties of Chemical Explosives. Prepared by the: Staff of the Explo-

sives Chemistry Sec. of the General Chemistry Div., Univ. of Califor-

nia, Lawrence Radiation Lab., Livermore, Calif. Rept. No. UCRL-14592,

AEC (contract No. W-7405-eng-48), Dec. 16, 1965.

Research on the Hazard Classification of New Liquid Rocket Propellants.

Prepared by: Rocketdyne Engineering. Rocketdyne, a div. of North

American Aviation, Inc., Canoga Park, Calif., Quart. Progress Rept.

for period ending Apr. 30, 1960, Rept. No. 2452-1, May 30, 1960,

67 pp. U.S. Air Force, Edwards, Calif. (contract No. AF 33(616)-6939).

Storable Liquid Propellants Nitrogen Tetroxide/Aerozine 50. Second Edi-

tion. Prepared under the direction of W. R. Fish. Aerojet-General

Corp., Sacramento, Calif., Liquid Rocket Plant, Rept, No. LRP-198,

June 1962.

Abstracts of Papers, Second AFOSR Contractors' Meeting on Chemical

Kinetics of Propulsion. Armour Res. Foundation of Illinois Inst. of

Tech., Sept. 11-12, 1961; Air Force Office of Sci. Res., AFOSR Rept.

No. 1417, 1961, 20 pp.

AFOSR Twelfth Contractors' Meeting on Liquid Propellant Rocket Combus-

tion. (Abstracts of papers presented.) Purdue Univ., Lafayette, Ind.,

Tech. Rept. 60-37, Mar. 2-3, 1960, 17 pp. Air Force Office of Sci.

Res., 1960.

Anhydrous Hydrazine. Olln Mathieson Chem. Corp., Industrial Chem. Div.,

Baltimore, Md., Mathleson Booklet I.D. No. AD-I061-558.

Anhydrous Hydrazine Handling and Storage. Olin Chem. Corp. Chem. Dive,

Nitrogen Produc_s, 745 FiTt_Av-e._ New Yor_, Olin Booklet

No. CD-140-464.

Apollo SE-8 Engine, Ignition Pressure Spike Testing. Rocketdyne, a div.

of North American Avlatlo=, Inc., Rept. No. BCI 65-109, NASA, 1965.

Bibliography: Part i. Satellite Attitude Control Systems.

Part 2. Thrust Vector Control Systems Second Injection. Part 3.

Adaptive Control Systems. Defense Documentation Center, Defense

Supply Agency, Cameron Station, Alexandria, Va.; Armed Services Tech.

Information Agency, Arli_ton, Va., Rept. ARt No. 13001, 1964, 31 pp.

Combustion Instability. Dynamic Sci. Corp.,Monr0via, Calif., Final

Tech. Rept. No. SN-1800, 1965, 74 pp. Report No. AFOSR 65-1683,

Air Force Offlce of Sci_-Res_ (contract No_ AF 49(638)-1i51).

73

822.

823.

824.

825.

826.

827.

828.

829.

830.

831.

III. Comparative Compatibility of Various Materials With Hydrazine and

Hydrazine Mixtures. Jet Propulsion Lab., California Inst. of Technol-

ogy, Pasadena, Calif., Memo. No. 20-152, pp. 3-4.

Dimazine; Unsymmetrical-Dimethylhydrazine Properties, Applications,

Reactions. F.M.C. Corp., Inorganic Chemicals Div., 633 Third Ave.,New York.

Evaluation of Combustion Instability Detector Techniques. (Supplement

No. A-I to Feasibility of an Optical Periscope for Use With Liquid

Rocket Thrust Chambers.) Final Report. Aerojet-General Corp., Azusa,

Calif., Rept. No. 3030, Tech. Progress Rept. for the period June 15-

Dec. 15, 1964_ May 1965, 61 pp. Report No. AFRPL-TR-65-44, Air Force

Rocket Propulsion Lab., Edwards, C ali-f_, Supplement A-I of contract

No. AF 04(611)-9703.

Liquid Propellant Safety Manual. Published by: Liquid Propellant

Information Agency, Applied Phys. Lab., The Johns Hopkins Univ.,

Silver Spring, Md., October 1958. Bureau of Ordnance, Dept. of the

Navy (contract NOrd 7386).

Monomethyl Hydrazine. Olln Mathieson Chem. Corp., Chem. Div., Baltimore,

Md., Mathieson Booklet I.D. No. AD-I198-361, 1961.

Monomethyl Hydrazlne Handling and Storage. Olin Chem. Corp., Chem. Div.,

Hydrazine Products, 745 Fifth Ave., New York.

Nitrogen Tetroxide. Allied Chem., Nitrogen Div., New York, ProductBulletin.

Storage and Handling of Dimazine (Unsym-Dimethylhydrazine). F.M.C.

Corp., Inorganic Chem. Div., 633 Third Ave., New York, Third Edition,26 pp.

Supercooling of Hydrazine. Naval Res. Lab., Problem No. C01-05, Proj-

ects RMMP 24-016/652-I/F 009-06-002 and RR 010-01-44, June 5, 1964.

Flaherty, Robert E. Impact Characteristics in Fused Silica for Various

Projectile Velocities. J. Spacecraft, v. 7, No. 3, March 1970,pp. 319-324.

ILl i] U 13 L[ I,,[ ILl U n LI Zi U JII, [\,

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