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US ARMY T

RESEARCH & DEVELOPMENT ACTIVITY

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METEOROWICAL DATA REPORT

BY

MARJORIE McIARDIE HOmALE

MX!H 1963 I 307 ERQA -294

‘30 (UTEQORYJ WAS* CR OR TUX O R AD NUMBER)

e

WHITE SANDS MISSILE RANOE NEW MEXICO

* -I

f GPO PRICE $

OTS PRICE(S) $

Hard copy (HC)

Microfiche (MF) 8

4

i

METEOROIJKICAL DATA REPOICT

m o m 3 NASA 4.56 GG (s/m NASA 133) (12 March 1965)

Marjorie McIardie Hoidale

.

.

Em-294 March 1965

_,-I-

-. .,

ABSTRACT

aW7 Meteorolwical data gathered for the

launching of Aerobee BASA 4.56 GG (S/N RASA 133) are presented for the National Aeronautics and Space Administration and for ball ist ic s tudies . The aata appear, along with calcul.a-ted bal l ist ic data, in Appendixes A, B, C and D. A dw

iii

B. A n e m w t e r Recordings of Wind Speed a d D i r e c - t i o n and Pilot-Balloon-Measured Wind D a t a f’rm the Surface t o 4,000 Feet - - - - - - - - - - - - - - - 7

13 C. Tables of Upper A i r D a t a - - - - - - - - - - - - - - - -

INTRODUCTION

A e r o b e NASA 4.56 GG (S/g RISA 133) WBS laanehed ~ ~ ~ l - & d m n c e assile Test &cili%y personnel, 'White Sands Missile" Range, New Mexieo, at 2038 hours ST, 12 March 1965.

t o predic t rocket impact were collected by the Meteomlogical Sapport Mvi- sion, U. Sm A m Electronics MSO~X€I and Dbwlapnsnt Activity, White Sands Missile Ran@, NOW Mexico. Gordon L. Dunaay and W j o r i e M. Hoidale.

Meteorological data used i n con junction w i t h theomtical calculations

The impact predictors for this f i r ing were

. Wind data f o r the first 4,000 feet above the surface were obtained

fran a I )o&le-~eodol i te Wind Velocity Computer System [I]. Balloons released a t t he launch site were observed and tracked fran a 2,000-foot baseline. Continuous angular data were transmitted from two e l e c t r i c a l l y instmmented theodolites t o a computer where the data we- reducod t o ob- t a i n a velocity-vs-height relationship, The canputor output drives tm, recorders which trace north-south and east-west caaponmts on a spe@ally designed wind velocity canputor b a l l i s t i c chart. I t is possible to mad d i rec t ly f im the chart both the man wind canponmt values and t he mom bal l is t ic wind caaponemts i n the various b a l l i s t i c layerr.

Tomper'atum, pressure and humidity data, along With upper wind data from 4 ,000 t o Ipproxipartely 75,000 fwt above tho surfam, wozw 6btrinq fmn standard rauinsonde operations,

Mom wind component values i n each b a l l i s t i c zane we= dotemined from vertical cross sections by the equal-area method,

Data qrpearing i n Appendix B am bued on the E, L, Walter [2] theory, n e "Pmdicted Impact" iacludes, & e n applicrble, an adjur tmnt 0% impact based on the exporicnrce of t h e imprct predic tor md the forecut of firing time wind condftionr,

m TABU OF BALLXSTIC FACTORS

AXROBEE I!?ASA 4.56 GG (SIR HASA 133)

-

. PAGE TABrzs - 4 A-I. Calculated Rocket Performance Values - - - - - - - -

3

APPENDIX A

TABLE A-1.

CALCULATED ROCKET PERFORMANCE VALUES

A E R m m NASA 4.56 GG (S/N MA 1331

UNIT WIND EFFECT Surface t o 2,000 FT 2.38 Miles/MPH (3)

WWER T I L T EFFECT

BURNOUT:

2,000 t o 100,000 FI! 4.28 Miles/hH 19 33 Miles /Degree

.

V e l o c i t y A l e i t u d e Tilpe

PEAK:

5,402 Feet/Second 122,338 Feet M L

51.0 Seconds

A l t i t u d e T i m e

110.8 Miles EL 220 Seconds

TOTAL TIME -OF FLIQiT 425 Seconds

CORIOLIS EFFECT (West) 5.05 Miles

*Includes Nosecone Weight

from 143 t o 2,000 feet . s t a t i s t i ca l studies.

(3)An empirical correction has been made t o the uni t w i n d effect This correction was determined from

Dunaway, G. L., "An Empirical Technique f o r Improving Aerobee- H i Impact Predictions," Meteorological Support Division, U. S. A r m y Electronics Research and Developnent Activity, White Sands Missile Range, Hew Mexico, May 1964.

4

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c

APPENDIX A

TABLE A - I 1

TABLE OF BALLISTIC FKNIRS

AER- .WWi 4-56 GG (SIET HASA 133)

HEIQiT INTERVAL BALLISTIC HEIQfT INTERVAL FEET FACTOR FEET

143 - 200

200 - 300

300 - 400

.lo0

.130

.lo2

.150

.078

.OX?

.018

.013

-012

5,000 - 10,000 - 15,000 - 20,000 - 25,000 - 30,000 - 35,000 - 40,000 - 45,000 -

10,000

15 ,000

20,000

25 , 000 30,000

35,000

40 , 000 45,000

50 , 000 1,600 - 1,800 .Oll 50,ooo - 60,000

1,800 - 2,000 .010 60,000 - 70,000

2,000 - 3,000 .os2 70,000 - 80,000

3,000 - 4,000 .040 80,000 90,000

4,000 - 5,000 .022 90#000 - 100~000

BALLISTIC FACTOR

0078

.&2

.030

.020

,017

.010

. 010

.006

*009

.010

.007

.006

.003

.a

5

_-

a

r

TABLES -

APPENDIX B

ANEMONE'ER RECORDINGS OF WIND SPEED AND DIRECITON

AND -

7

A-IX B

TABIrE B-I

ANEMCMETER RECORDINGS OF WIND SPEED AND DIRECTION

AEROBEX NASA 4.56 GG (S/N NASA 133)

!MME WIm SPEED 0 (Kmcrrs> T - 15 19.0

T - 10 17.5

T - 5

T - Time 17.5

15 .O

T + 5

T -+ 10

16.5

17.0

T + 15 17.0

DIRECTION (DEGFEES)

NOTE: Wind speeds and directions are 5-minute averages centered a t indicated times

8

9

TABU B-I1 (Cant)

.nM = Missing

10

.

c

11

TABLE B-EI (cont)

TABLES OF UPPER AIR DATA

aER0BEE HASA 4.56 GG (S/R NASA 133)

C-I . Mean W i n d Components for Ballistic Zones (4 ,000to20,000Fet) - - - - - - - - - - - - - - - - - - - Mean Wind Components for Ballistic Zones

14

C - 1 1 . (4,000 t o 1 0 0 , ~ Feet)- - - - - - - - - - - - - - - - - - - 1 5

16 C - 1 1 1 . Upper A i r Data (Release Time: 1420 M3T) - - - - - - - - - - C-IV.

C-V.

Upper A i r Data (Release Time:

Upper A i r Data (Release Time:

1650 ET) - - - - - - - - - - 2038 ~JSTO - - - - - - - - - -

22

28

APPENDIX c

RELEASE NO. REmSE TIME

TABLE C-I

UPPER A I R DATA

AEROBEE NASA 4.56 GG (S /N NASA 133)

MEAN WIND COMPONENTS FOR BALLISTIC ZONES IN IU"S

1

(MST)

LSLYEFE IN FEET

1923

N-S E -W

4,000 - 5,000

14

25.W 9.0s I

APPENDIX C

TABLE C - I 1

UPPER A I R DATA

AEROBEG NASA 4.56 GG (S/X HASA 1331

MAN WIND CWONENTS FOR BALLISTIC ZONES IN KWIS

1 .

2 3

1650 I 2 8 I E-U 1 N-S N -S E -U N-S

2.55 8.01 3 =os - 18 .o

4,000 - 5,000

5.000 - 10.000 6.0 10.5

ll.5 32.0 1 2 . 5 34.0 6.0

57.0 5.5

83.0 4.5

91.0 9.0

llg.0 22.0

101.0 8.0

31.5 1 10,000 - 15,000

15,000 - 20,000

20,000 - 25,000

25.000 - 30.000

16.5 45 .O 10 .o 46.5 I 52.0 30.0 -

33 -0

21.0

7

64.5,

88.0

104.0

99.0

93 -0

61.5

22.0

.

I

8.5

2 .a 0.0

38.0

43 .O - 30,000 - 35,000

87.5 - 18 .o 32 .o - 35,000 - 40,000

40.000 - 45.000

24.5 10 .o 45,000 - 50,000

50.000 - 60.000 16. on 6 . a 60,000 70,000

70,000 - 80,000

80,000 - 90,000

90,000 - 100,000

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33

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... .

. .

APPENDIX D

.

35

APPENDIX D

TABU D-I

IMPACT PREDICTION DATA

R ='Rawinsonde Winds (Above 209000 Pt.1 R1 = Rawinsonde Winds (4,000-209000 Ft) R2 = %win Winds (4,000-20,000 I?%)

*Post-Shoot Data 36

APPENDIX D

TAB= D-I (Cat)

IMPACT PREDICTION DATA

AEROBEE ETAsS4.56cK: SERIAL 80. RASA 133

JACX SETTINGS

West leg 69 inches E a s t leg 5 i n d e s

T i l t 7.26 , degrees Azimth 055.5 * m s

CoMp(HENTS OF TILT&

4.11 dsgmes north 6.08 dsgrws east

NO WIND IMPACT

100.3 miles east of Navy Blockharte - 69.8 miles north of Navy Blockhouse - PREDICIZD IMPACI'

5 niles west of Navy Blockhouse - 50 miles north of Navy Blockhouse

PREDICIED BOOSTER IMPACT

AzimUth 055 degrees Distance 2,500 h o t

Recamtendation lo fire

W i t h 65 I confidence o f impacting on range, bared upm: <

wind correction 107 lniler

one hmr wind variability 10.5 adlrr

f D8-/ThO 12 Mch 1965/2027 BST

Actual

Actual

.nsonfc

IIpact ( P m r Lamchar) 59.4 miles north, 7.8 miles west (S6na)

Boostor Impact (Pram Lamchor) H/A

Observation of Trajectory and Impact of Missiles 37

a

t

Approval. Data Report ERDA-294 has been reviewed and approved for publication :

Acting Chief Meteorological Support Divfs ion

MaJor, signa# Copps Director Environmental Sciences Directorate

Distributione !This report has been distributed i n accordance with SEEWS-E In fa t No. 1. I n i t i a l printing 84 copies.

38

1. D a t a Report Em-294 has been prepared under the supervision of the Metearolcgical Support Division and is published for the information and guidance of all concerned.

2. Suggestions or criticisms relative t o the farm, contents, purpose, or use of this publicaticm should be refemed t o the Catwanding officer, U. S. Army Electronics Research and Develapment Activity, A m : White Sands Missile Range, XewMexico.

SXIS3-Z,

2d Lt, AGC

.

/ Assistant Adjutant

4

39