UNCLASS;i V!u · 2011. 5. 13. · R(M) is the spectral responsivity of the detectDr in V W'1 m-I 1...
Transcript of UNCLASS;i V!u · 2011. 5. 13. · R(M) is the spectral responsivity of the detectDr in V W'1 m-I 1...
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UNCLASS;i V!u
UNLIMITED DISTRIBUTION
CRDV RAPPORT 4233/81 DREV REPOR-T 4233/81
DOSSIER: 3633H-039 -FILE: 36331-039SEPTEMBRE 1981 SEPTEMBER 1981
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DETECTION RANGE PROBABILITIES OF
P:\SSI E INFRARED SYSTEMS FOR TIHE NWIRTIT ATI.ANTIC
A. Laflamme
OEC 2 3 1981 "
BUREAU - RECHERCHE ET DEVELOPPEMENT RESEARCH AND DEVELOPMENT BRANCHMINISTERE DE LA DEFENSE NATIONALE NON CLASSIFIEf DEPARTMENT OF NATIONAL DEFENCE
CANADA DIFFUSION ILLIMITEE CANADA
81 12 23 110
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CRDV R-4233/81 UNCLASSIFIED DREV-R-4233/81DOSSIER: 3633H-039 FILE: 3633H-039
DETECTION RANGE PROBABILITIES
OF PASSIVE INFRARED SYSTEMS
FOR THE NORTH ATLANTIC
by
A. Laflamme
CENTRE DE RECHERCHES POUR LA DEFENSE
DEFENCE RESEARCH ESTABLISHMENT
VALCARTIER
Tel: (418) 844-4271
Qu6bec, Canada October/octobre 1981
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RESUME
En s'appuyant sur les probabilit6s d'extinction du rayonnement
infrarouge dans l'atmosph~re, on pr6sente les probabilit6s de distance
de d6tection de cibles par les syst~mes passifs de surveillance en
infrarouge. La zone g6ographique d'int6rSt est l'Atlantique nord.
On considbre les 2 principales fenStres atmosph6riques dans l'infra-
rouge, les bandes de, 3 1 5 et de 8 1 12 micrombtres. Les r'&ultats
permettent de pr6dire et de comparer rapidement la performance des
systbmes de d6tection. (NC)
ABSTRACT
Bad-,on probabilities of extinction of infrared radiation in•,the atmosphere, range probabilities for target detection by passive
invrared surveillance systems are presented. The geographic area
covered is the North Atlantic. The two major atmospheric infrared
windows, the 3 to S and the 8 to 12 micrometer bands, are considered. iiThe results allow to predict and compare readily the performance of
detection systems. (U),/
PC __ __ _
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TABLE OF CONTENTS
REiSIJE/ABSTRALCT .. . . . . . . . . . . ... . . . . . . . . .
1.0 INTRODUCTION..................................................1
2.0 MATHEMATICAL FORMULATION ..................................... 1
3.0 LIMITATIONS .................................................. 4
4.0 DETECTION RANGE PROBABILITIES ................................. S5
50CONCLUSION ................................................... 7
60ACKNOWLEDGMENTS .............................................. 8
7.'REFERENCES ................................................... 9
TABLE I
FIUE o7
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1.0 INTRODUCTION jA previous report proposed a simple model for the extinction
of infrared radiation in the atmosphere (Ref. 1). This model was
used in Ref. 2 with the probability data of the pertinent meteoro-
logical variables as derived from measurements made by Ocean Weather
Ships to compute probabilities of infrared radiation extinctions in
the North Atlantic.
In this report, these extinction probabilities are used to
compute range probabilities for detection/tracking with passive systpms
in both major atmospheric iR windows, the 3.4 to 5.0 micrometer and
the 7.75 to 11.75 micrometer bands, hereafter called the 3 to 5 and
the 8 to 12 micrometer bands.
This work was performed at DREV between March and June 1981
under PCN 33H39 Electro-Optical Fire-Control Tracking Study.
2.0 MATHEMATICAL FORMULATION
The signal voltage produced by a passive detection system can be
described (Ref. 3) as:
Vs f JC() T (X) T (X) R(X) dX [1]r X
where V is the the peak signal voltage in V,
A is the area of the entrance aperture of the optics in cm 2
r is the range to the target in cm,
J(X) is the spectral radiant intensity of the target in W sr pm
T a() is the spectral transmittance of the path (dimensionless),
iia
Lr_--
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T o() is the spectral transmittance of the system (dimensionless),
R(M) is the spectral responsivity of the detectDr in V W'1 m-I
1 and X2 are the limits of the spectral interval of the sensor
in jim.
t To simplify [1], it is customary to convext the wavelength-dependent terms into their integrated values over the bandpass of the
sensor. Effecting this and dividing both sides of the equation by Vn,
the rms noise from the sensor system, one obtains:
Vs =[A Tn RI|JJT | IS -2n-I +
where S is the signal to noise ratio.
By definition, the Noise Equivalent Irradiance (NEI) is the
irradiance at the entrance aperture which produces a peak signal equal
to the rms noise, i.e. S = 1. Since the second bracketed term in [2]
is the irradiance from the target, then for S = 1,
VNEI = A T R [3]
and [2] can be written
TJ a
NE-I" -2 [4]
r-2
in which NEI is the noise equivalent irradiance of the system in W cm
J is the radiant intensity of the target in W sr ,
S is the required signal to noise ratio.
I.°.
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The transmittance of the path from the target to the sensor has
the following form:
Ta -0 tr [S]
where at, the total extinction coefficient in km-, is the sum of 3
components:
t = a +a +a [6]
in which a is the extinction due to aerosols, in km"-
a is the extinction due to rain, in km-,
am is the extinction due to molecular absorption, in km-
Both aa and ar are relatively independent of A and their average
values can be used readily. On the other hand, am varies rapidly with
A and the use of a single average value would introduce appreciable
errors in the calculation of Ta for different path lengths. Laflamme
and Corriveau (Ref. 2) computed and average value for am at a fixed
range of 10 km (amlO) and multiplied it by a function of range (FR) as
a range correction factor. Thus
FR x [a]am •mlO
By-substituting [5], [6] and [7] in [4], we obtainj e-(a + a + FR x a )r
1=__ __ _ e a r m(810= 2 181So NEI x 100r
'1,
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UNCLASSIFIED
in which the factor 100 has been introduced to express the range, r,
in km rather than in cm. The next equation is easily derived from [8]
K = loges.NEl O) a r FR x )r + 2 loger [9]SNIx 10lO =(a+a m
K is a single number which characterizes the engagement, namely
the target by its radiant intensity, J, the sensor by its noise equiva-
lent irradiance, NEI, and by the signal to noise ratio, S, required to
obtain a desired false alarm rate.
The extinction probabilities computed in Ref. 2 were used to
calculate the probabilities of detection ranges by solving [9] for
the range, r, with K as a pprameter. The results can thus be applied
to any passive system whose operatiu,.. zan be described by the above
equations.
3.0 LIMITATIONS
In this previous discussion, the noise has been taken as system
noise only and any extraneous noise signal generated by the background
(clutter) has been neglected. Supplementary processing performed by
the sensor system for the extraction of the target signal from clutter
could possibly be assimilated to an increase in the signal to noise
ratio, S, required and/or a delay in the target declaration. The detec-
tion ranges calculated in this report are then maximum ranges, as ob-
tained against a clutter-free background. The clutter-induced reduc-
tion in detection ranges cannot be evaluated properly at this time
because of the lack of statistical data on the clutter intensity and
spatial distributions. Furthermore, this reduction will depend on
the degree of sophistication of the sensor signal processing scheme.
is __ _ _ _ _ _
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I UNCLASSIFIEDA further restriction is that the model used provides extinction
coefficients for horizontal paths near sea level. Since the extinction
usually decreases with altitude while the signature of the target may
become stronger due to an improved aspect angle, the calculated
detection ranges should be even better for slant paths. On the other
hand, the higher the target, the greater are the chances that the path
between sensor and target will go through clouds, which would shorten
ranges considerably. This last effect has not been evaluated, again
because suitable statistics on cloud frequency, type, ceiling, etc.
are not available presently.
4.0 DETECTION RANGE PROBABILITIES
The extinction probabilities presented in Ref. 2 were based
on the measurements of meteorological parameters collected by Ocean
Weather Ships. Table I lists the locations of the ships and the
period of observation covered. Each location is identified by a
letter and all are in the North Atlantic, except for N and P whichare in the Pacific. The extinction probabilities were used with
equation (9] to compute detection range probabilities with K as
a parameter, so that any engagement between a given sensor and a
given target can be studied with the curves presented.J
The detection range probabilities have been computed for both
the 3 to S and the 8 to 12 micrometer bands and each figure presents
2 sets of curves, each set applicable to one band in a corresponding
location ane season.j
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UNCIASSIFIED
TABLE I
Weather Ship Locations
OWS Ident Period of Record Position Limits
A 1964 - 1971 61.0-63.0 N, 31.0-35.0 W
B 1965 - 1972 55.5-57.5 N, 49.5-52.5 W
C 1965 - 1972 51.5-53.5 N, 34.0-37.0 W
D 1965 - 1972 43.0-45.0 N, 40.0-42.0 W
H 1970-present 35.0-37.0 N, 47.0-49.0 W
I 1964 - 1971 59.0-61.0 N, 18.0-21.0 W
J 1964 - 1971 52.3-54.3 N, 17.8-20.8 W
K 1964 - 1971 44.0-46.0 N, 15.0-17.0 W
M 1964 - 1971 65.0-67.0 N, 0.0 - 4.0 E
N 1965 - 1972 28.5-31.5 N, 138.0-142.0 W
P 1965 1971 48.5-51.5 N, 142.6-147.6 W
Figures 1 to 44 show the detection range probabilities for each
of the 11 locations and each season. Figures 45 to 55 refer to the
same locations but present yearly averages.
A
The locations have also been grouped in 4 regions:
- locations A, B, C, and M, North of the Gulf Stream;
- locations D, H, J and K, in thL Gulf Stream;
- all locations above, or the North Atlantic;
- locations N and P, Pacific.
S• "'' • '•" .. ... . . .... I.... - -' • . . ..- ' r W •
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UNCLASSIFIED7
Figures 56 to 71 show the detection range probabilities averaged
for each region, season by season, while figures 72 to 75 present
regional yearly averages.
Each figure is properly identified and should be relatively
easy to use. As an example, for a surveillance system having a NEI of
10 W cm working against a target with a radiant intensity,
J, of 3 x 32W sr- and requiring a signal to noise ratio, S. of 7,the value of K would be
1 2K -log ~ 3= 09.06
The detection range probabilitiy for a given location (or region)
and season can then be read directly for K =9 on the appropriate
figure.
5.0 CONCLUSION
By using IR radiation probabilities derived from meteorological
measurements made by weather ships in the North Atlantic, detection
range probabilities have been computed which are applicable to most
passive IR systems in both the 3 to S and the 8 to 12 micrometer bands.
Although the accuracy of the results is limited by some factors
such as the adequacy of the extinction model, the presence of intervening
clouds, and the effect of background clutter, the curves presented
readily supply reasonable estimates of the expected performance of
I IR surveillance systems and would be even more precise as a toolto establish the relative merits of various systems.j
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6.0 ACKNOWLEDGMENTS
The author wishes to thank Mr. R. Corriveau for his enlighteningcomments during the preparation of this report.
ii
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7.0 REFERENCES
1. Corriveau, R. and Laflamme, t,., "A Simple Atmospheric ExtinctionModel for Infrared Radiation" (U), to be published.
2. Laflamme, A. and Corriveau, R., "Probabilities of Extinction ofInfrared Radiation for the Northern Atlantic" (U), DREV R-4216/81,UNCLASSIFIED
3. Hudson, Richard D. Jr., "Infrared System Engineering", John Wiley& Sons, Inc, New York, 1969.
:4,
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48
PROP. LOC. N
1.0 FALL
.0
t2
.0 o0.0 20.0 .0 a 41.0° 0o.0
3-5 I1ICROI1ETER RANGE < Kl >
PROP. LOC. N
1.0 PAL L
4.
LS
,.\L
.0 1,0.0 20 0 S0 a 1.0 . a 60.0
6-12 0I'CROIETER RANGE NICI1,
FIGURE - 39
-
UNCLASSIFIED49
PRO&. .Oc. Ni
ZINTER
1.0
.6
.2
.0 .1•0.0 20.0 30.0a •.0 560.0
9-- iiICROI1ETER RANGE CKH>
PROF . LOC. N
1.0 ZINT.XR
.4
.6
\1 2
.0 .10.0 20.0 30.0 1+0.0 60.0
6-12 JllCROffX7*XM RANCE CK0N>
FIGURE- 40
______
-
UNCLASSIFIEDso
5O5
PRf'OPn. LOC. P
.8
IL .4S. NG ,1' .2 _____
.2-
1.0 _ _ _ _ 0_ _. _ _
.0 .1.0.0 20.0 30.0 4. .0 50.0
3-6 IIICRO/IETER RANCE
PROP. LOC. P
...
.\0
.0 .10.0 20.0 90.0 4•0.0 50.0
6-2.2 oJicRmflSTem RANCE CKJ>
FIGURE = 41
ILJ
-
UNCLASSIFIED51
PROP. LOC. P
1.0 S0flYIIXR
•.L
.2 3
.0 .1.0 0 20.0 So.0 4.0 0 50.0
3-5 I1ICROffETRR RANCE 1
PROF. LOC. P
1.0 E___SJlfR
.6L 2
.22
FIGURE - 42
.1!.
II
-
UNCLASSIFIED52
PROP. LOC. P
0FALLL
.6
lo a L 20 .o 30 . a w0. 0 0 . 0
'- 3-6 "ICRO"ETER NANC.E
SPROP. I..Oc . P
.6 :!
.4.
3
.0
.0 .10.0 20.0 30.0 o.0. 50 s.0
6-12 01CROI1~TER NANCE CKNI>FIGU. - 43i
.6 .1.
. 0 .1.0.•0 20 .0 30 .0 40. 0 50 . 0
8-.L2 I1ICRO11E2"ER RANGE CKN)
FIGURE - 43
I __.__
-
UNCLASSIFIED53
PRO&. L.OC. P
1 07B~
.LS
.0 .2.a.0 20.0 30.0 '40.0 60.0
S-6 "hICRONETE.R RANCE
PROP. 49GC. PLr I NTAR
.0 3.0.0 20.0 :90.0 '40.0 50.0
6-2.2 "1!cso"E1sTA XANGE CKM>
FIGURE -44
-
UNCLASSIFIED
P~roD. L.OC. A
1. ____SPRIN4 5&/flER FAL.L t~rI N7*ER
.LS
L2
.2
a0 10.0 20.0 30.0 V 0. 50.0
3-6 nICRO1E~TER RANCE
PiRODr. LOC . A
1.0 NPM dM4 srJIjlERm FA.LL UINT1EM
14.0
.2
.0
.0 10.0 20.0 30.0 4.0.0 50.0
6-12 "IICROJIETER RANCE ICKH)
FIGURE - 45
-
UNCLASSIFIED55
PROD. LO. o USPNItJG SOONEfR FrALL I- vTER~
1.6
L4
.62
.22
.0 .10 .0 20.0 so.0 4.0.0 50.0
3-S Lo ftCO fE RJ4 K~
1. ____SPRING SOONIER FALL UrINTER
.6D
.0 1 .0 0.0 0.0 40.0 50.
01RM.' RNECN
FIGURE 4
-
UNCLASSIFIED56
PROF. LOC. C
1. 0 SPRING s.UJflER FALL ErINTER
J.. __ _ _ _ _ _ _ _ _ _ _
.2
.0 _ _ _ _ _ ._ _ _ . _ _ _
a0 10.0 20.0 30.0 4+0.0 a 50.0
9-s oICROffeTeR RANGE CKit>
PROP . LOC . C1. 0 SPRING SfJINJER FALL WINTER
.8 __,___
.4*4
.0 .10.0 20.0 30.0 40.0 60.0
8-1.2 fficRofIfTER RANCEK -4>
FIGURE - 47
_~~ 7-. z__
-
UNCLASSIFIED57
PROP. LOC . p
1.0 SPRING SOONER FALL E ZrINTER
J..
.0 .1.0. 20.0 So . a 0 . a 50.0
9.-6 "£cso"E£rs RANCE •
PROP. LOC . vSPRINCG SOJONE1R FAL-L. ErJNrctR
12
k.44
. 0 ____ __ _ __ __ _ 0.0 .1.0.0 20.0 30.0 40.0 so. 0
6-,.2 if1cRov"ETR RANGE CKff>
FIGURE - 48
L .., ..
-
UNCLASSIFIED58
PRO&. LOC. 8
1. a sPRmNG. SoifflER FALL XrXNKER
J..O
.22
.0 _K'_ L
1 . .0.0 20.0 30.0 0+0.0 50.0
3-5 I1ICROff8'TE•R RANGE
FIGURE - 49
-
UNCLASSIFIED59
PROP. LOC. I
*0SPRING SOONEI~R FALL..r TIIN 79R
.0 10 0 2 . 0 0 W .a 5 .
1.0 SRN ONRPILtI7s
.0 .10.0 20.0 30.0 4+0.0a 50.0
6-12 fICROM~Erc RANGE~ (XII
FIGURE 5
-
UNCLASSIFIED60
PhROF. £OC. J
SPRING SUrMNER FA" 4 rINTWR
.,61 0
1.0
4 .0 10.0 20.0 30.0 4o0.0 50.0
K-12 #ICRONE1TER RANCGE CKt3>
FIGURE - 51
PRF LO..
-
UNCLASSIFIED61
PROD. LOC. K
- • 0 SPRING SYIMMER rA.L - TrINT"ER
NL2
.0 .10.0 20. 0 0.03 a 0 0 a 0.0
S-S2 tICROffETER RANGE
4 -~PROP. LOC. K
1.0______SPRr114 SOONE IIR PA44 A INTrX
FIGURE - 52
141.6!
-
IUNCLASSIFIED62
PROP. LOC . )v
SPRtN4 SCIIIISP FALL. WIrNtKR
1.0I!
.2
.1.0 .1.0.0 20.0 S0 . 0 L0•. 0 so . 0
6--2 "ICROIffETER RANCE CKN>
.FROG. LocE. -5i,• ~3?RIzN• StJNNR FALL. r•r!NER
i " I
.0O .t.0.0 20. 0 30. 0 4O. 0 50. 0
i FIGURE - 53
-
UNCLASSIFIED63
PROP. A.OC. NSPRING Su/il ER FALL tIJ'NTXR
AS
.4 \L2.2.
a X-
.0 .10.0 20.0 30.0 4.0.0 60 . 0
:9-6 IIICROIerTEm RANCE (KNM
PtROp. LOC. NSPRING SImNER FALL UriJNTER
•L 1II L
-1
0 ,10.0 20.0 30.0 40.0 50.0
8-.2 IIJCROIIETER RANCE C•HC>
FIGURE -54
I -
-
- - J
UNCLASSIFIED64
PROD. t.OC. P
1.0 SPRING SOONEIR FALJL. ,rrUItR
S1-6 _JCOErrm RANCE
-
w
UNCLASSIFIED65
PROP. LOC. ADCIII* $PRINC
S£4.
3
* �.. 2
.2
.2.
.0
.0 .1.0.0 20.0 30.0 4.0.0 50.0
3-� J1ICROI1�TE�k RAN�r (Kil>
PROF. L�C. AFC 111
SPRf�
.0 1.2.
I
4.0 .0 .1.0.0 20.0 30.0 40.0 50.0
6-1.2 PIt CROP! UT UK RA�U (Kif)
FIGURE - 56
'I . -a-.. -
-
UNCLASSIFIED66
PROP. £OC. ANC I I
1.0
10 . 200 20.o 90.0 w0.0 50.0
S-~ 1IC~ffT~RRANCE
PROP. £.Oc. AOd?!
1.6
.4 a2
.022 . 3 . f a a S .
6-12 NICROM.e."RANCE CKM
-
UNCLASSI FIED67
PROS. ILOC. ANC II
1.0
~~~0.0 30.0 2o o o 40 .0 o.o
3-5 NCROI~T~RRANCE~
PROS. £OC . APCIII
* ____ _ PALl
.0020 0. o0s.
6-12iyicojyjrxx ANCECK1.
.IUR6-5
-
UNCLASSIFIED68
PROS. LOC. ADC I
. 0 _ _ _ rINT ER
ti
i.4. 2
.2
10.0
•.0 .0 .0 2 .0 3:0 . 0 4.0.0 51:3.0
3-,i.6 ,•hICROI.&TEJ RANGE£ CKNI>
PROP. Loc. AFIN
1. ____WIN7rc
.2_
.0 3.0.0 20.0~ 30.0 +0 . a 50.0
a-.le NICROIIETER RANGE (XII)
FIGURE - 59
-
UNCLASSIFIED69
PROF. 4OC. DRJX
INPR'N
L S
.I..
.2
.0 10.0 20.0 30.0F 0.E0 -0.0
6-12 01CRONF.T&S RANCE CKit)
PROFGUR 60C P4
-
UNCLASSIFIED70
PROD. .. OC. D*JK1. . It/U•IER
L.6
.84..6
.1+
.L2
.0 1.0.0 20o.0 so . 0 4+0.0 •0.0
3-6 miICRONETER RANGE CKN>
PROP. • OC. DNJK
.4.
0 . 0 . 0 20.0 30.0 wa. a 0.0
6-1.2 I01CROIIETER RANGE CXK>
FIGURE - 61
-
UNCLASSIFIED71
PROP. LOC. PJXFALL
.2
•.0 .10.0 20.0 30.0 Wo0.0 50.0
3-• I/ICROI1W2EWR RANGE CKIF>
PROP. LOC. DRrxK
1.0 FALL
.14.1
.01
.0 ,.10.0 20.0 30.0 o . 0 50.0
6-J.2 fICROITE"'£R RANCE CKff>
FIGURE - 62
Li __
-
UNCLASSIFIED72
PROP. L.OC. psix
VINITER _ _ __ _ _1.0
.22
.0
.0 10.0 20 .0 30.0 '.0 50.0
3-6 MICRONfT£R RANCE CKff>
PRON. LOC. NJKX
.90
.0 __ _ _ __ _ _ _ __ _ _ _ __ _ _ _
.0 10.0 20.0 30.0 4'0.0 50.0
6-12 .IICROVETBR RANGE CKN>
FIGURE - 63
-
aI
UNCLASSIFIED73
PROP. L.OC. ACIIMDMJK1.0. ____SPR J"NG ___ ___
.8L 6
.4-
.22
.• 0 ____ _ __ _ _0 \_ .1.t •.0 a1.0 20.0 30.0 4-0.0 50.0
3-6 M1ICROlYETER RANGE CKV >
PROM. LOC. ANCIMDRK
1. SPRIN4G
.6 ±
0
.0 10 0 20 .0 30.0 '4.0 0 50.0
6-12 hINCROmrETER RANCE K•(?>
FIGURE -64
F' • •*•
I I I I I i' I-
-
UNCLASSIFIED
.22
.0 0.0 20.0 30.0 '40.0 50.0
3-6 HIICRO11ETER RANC~E
PROP. LOC. AffclmvDHJK
.6L 2
.2
.0 ±0.0 2 0. 0 s0.0) 9+0.0a 50.0
8-12 "IICRC'IETER RANCE CKit)
FIGURE -65
-
UNCLASSIFIED75
PRON. LOC. AsC.iIDRJKFALL _
1.0.
.4IL 2
0 1.0. 0 20.0 30.0 W4. a 50.0
3-- nICROMIETER RANGE 'Kff>
PRO&. LOC. ANCIMIPH-JI
1.0 _FALL
.4 . _L
.0
.0 10.0 20.0 30.0 40.0 50.0
6-1.2 IoxCROITEn"R RANGE CKM>
"FIGURE - 66
-
-77-
UNCLASSIFIED76
P*ROP. Z.~N~ORC. ANCIIIDNJK
1.0
L2
.0 3~10.0 20.0 30.0 WO~.0 5.
9-s ROIE iycm#sft RANCE 'CKH>
PRO&. LOC. ANCIIIDmJx
1 .0 _ _ _ _ __ __ ___ __ __ __
.2
K.0 10.0 20.0 30.0 40.0 6.
8-12 I7!CROZIErER RANCE ICKM)
FIGURE -67
-
-- "" NE-W-
UNCLASSIFIED77
PROP. LOC. PN
1.0
.2 2
.0 .0.0 20.0 $0.0 .0.0 50.0
3-6 MIICROMIETER RANGE CKV>
PROP. LOC. PN.11. OSPf'RI/NG.
., I \ \, I
II
.0 .0.0 20.0 $0.0 40.0 50.0
6-.2 MJICROMErTER RANGE CKI>
FIGURE - 68
* . 1 .. ... . . ... -••,
-
UNCLASSIFIED78
PROP. .OC. PN
3.0 __ _ _SViIIIIER
.2L
.0 300 20.0 30.0 4.0.0 a 50.0
6-12 IICROIIETEM RANC~E CKf>
PROIGUR -C 69
-
UNCLASSIFIED79
PRO&. LOC. PNFALL.
4S°9
.0 .10.0 20.0 3. 4 .0o. 0 S.0
3-6 H1!CROiETER RANGE CK1.>
PROP. LOC. PN
10 FALL
.L
. 10.0 20.0 30.0 40.0 60.08-1.2 /YlCROIIETER RANGE (Kff >
FIGURE - 70
-
UNCLASSIFIED80
PROP. LOC. PN1.0 _____KINTWR
L 6 9f
.8 39
L2
• .0 .0..0 20.•0 0.a 500 .0
3-6 oiCRO"ETER RANGE
PROM. LOC. PN
".a ____ xNrc
.o .__ __ _., __
.0 10.0 20.0 30.0 4•0.0 60.0
6-12 01ZCROI1ETER RANOR CKX>
FIGURE - 71
-
- . 2 - -- -_-
UNCLASSIFIED81
PROP L.OC .Apc IN
PROP. LOC. ANCIII
SPR.NG. $O•/4sa R FALl. TrrINTER
J..2
.0 .1.0.0 20.0 30.0 1+0.0 60.0
3-2 rf ICROMIETER RANGE
P'RO . t GOCE. A 7CIj.o___SPRIrNG $•JfI1YE, FA£l.- 1'INTEr',
•.8
S3\I
.0 .1.0 .0 2 0 .0 30.•0 4 0. 0 50 .•0
FIGURE - 72
-
.. .t =77...
UNCLASSIFIED82
PROB. 4OC. DHJKSPRING SCJIIIER FAL1 TIrINr"ER
I.8
4.
2 I N2
.0 _ _ __"_ _ _ _ _-_ _ _ _
.a 10.0 20.0 30 .0 040. a s 0
3-6 II"CRO.IETER RANCE CK?1>
PRON. LOC . DN..KSPRING saIIYIER FALL ITUI NTSER
.6 -, 2
.2 ±
0 0.0" 20.0 :3,0 0 •. 60. 0
8-12 IfICRO'IETER RANGE CKN>
FIGURE - 73
-
UNCLASSIFIED83
PRQD. £OC. ANCIJIDSJK
1.0 SPpRNo SaJI1I1 FALL UJIN7'XR
.4L2
.0 .20.0 20.0 SO.0 a 0. LF 50.0
3-6 01JCROI1ETEM RANCE CKif>I
PRiOp. 40C ABC IIIDJK
t. a _ _ _ SPRIN G StJIWER FALL. VXrZN~ r I
.2
.0 10.0 20.0 SO5. 0 8410.0 50.0
8-12 PIICNO1IETr~i RANGE CKI> I
FIGURE - 74
-
UNCLASSIFIED84
PROP. 40C. PM
1.0 SPRING SOOINIIER FALl. r I NTXR
.. 2
L2
.0 10.0 20.0 30.0 4•0.0 so.0
3S-6 MICROME2TER RANGCE CKM>
ROF. .LOC. PN
1.0 SPRrNG4 SOONJIER FPALL,.- ?rhrNtr".
.2 L I
.0 __ __
.0 10.0 20.0 30.0 9+0.0 50.0
8-12 MIICROMIETE.R RANCE CKtJ)
FIGURE - 75
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