PHOTOGRAPHIC EVALUATION REPORT MISSION 1004-2 19-22 FEBRUARY 1964

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• Collection: NGA Records (Formerly NIMA)
• Document Number (FOIA) /ESDN (CREST): CIA-RDP78T05439A000500050005-0
• Release Decision: RIPPUB
• Original Classification: T
• Document Page Count: 46
• Document Creation Date: December 28, 2016
• Document Release Date: April 1, 2002
• Sequence Number: 5
• Publication Date: June 1, 1964
• Content Type: REPORT

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65 Pages
TECHNICAL PUBLICATION
PHOTOGRAPHIC EVALUATION REPORT
MISSION 1004-2
19-22 FEBRUARY 1964
Declass Review by NIMA/DOD
WARNING
This document contains classified information affecting the national security of the United States within the
meaning of the espionage laws U. S. Code Title 18, Sections 79.3 and 794. The low proh?ibits its transmission
or _the revelation of its contents in any manner to on unauthorized person, as .well as its use in cny manner
arejudiciRf to the safety or interest of the United States or for. the benefit of cny foreign government to the
detriment of the United States. It is to be seen only by personnel especially indoctrinated and authorized to
receive TALENT-KEYHOLE information. Its security must be maintained in accordance with KEYHOLE and
TALENT regulations.
NATIONAL PHOTOGRAPHIC INTERPRETATION CENTER
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TECHNICAL PUBLICATION
PHOTOGRAPHIC EVALUATION REPORT
MISSION 1004-2
19-22 FEBRUARY 1964
NPIC(TP-17/64
June 1964
NATIONAL PHOTOGRAPHIC INTERPRETATION CENTER
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TABLE OF CONTENTS
SYNOPSIS
GENERAL FLIGHT DATA
PART I. CAMERA OPERATION
;
1. Master (FWD) Panoramic Camera 1
9. Slave (AFT) Panoramic Camera 2
3. Master (FWD) Horizon Cameras 2
4. Slave (AFT) Horizon Cameras. 2
-5. Stellar Index Camera 3.
6. Terrain Index Camera 3
7. Collateral Equipment 3
PART II. FILM 3
1. Film Processing 3
2. Film Degradations 4
PART III. IMAGE QUALITY 6
1. Photographic Interpretation Suitability 6
2. PI Suitability For Mission 1004,2 6
'3. Mission Information Potential 7
4. .MIP For Mission 1004-2 ? 8
APPENDIX A. _SYSTEM SPECIFICATIONS
-?APPENDIX B. TECHNICAL COMPENDIUM 13
- APPENDIX C. DENSITY READINGS - 17
APPENDIX D. EDGE SPREAD FUNCTION .24
APPENDIX E. MISSION COVERAGE STATISTICS 29
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FIGURE
FIGURE
FIGURE
FIGURE
FIGURE
FIGURE
FIGURE
FIGURE
FIGURE
LIST_ OF ILLUSTRATIONS
Page
1. SOFT IMAGERY 2a
2. CORONA STATIC AND FREQUENCY MARKS IN THE
FORMAT 2b
3. ROLLER SHADOWGRAPH AND FREQUENCY MARKS
IN THE FORMAT 2b
4. SHORT EMULSION SCRATCHES ADJACENT TO THE
CAMERA NUMBER 2c
5. RANDOM LONGITUDINALEMULSION SCRATCHES
6. RAIL SCRATCHES 2d
7. HORIZON IMAGERY AT SOLAR ELEVATION 50
8. HORIZON IMAGERY AT SOLAR ELEVATION 18? 2f
9. HORIZON IMAGERY AT SOLAR .ELEVA7FION 42?
SHUTTER REWIND MECHANISM MALFUNCTION AND
EDGE STATIC, STELLAR INDEX CAMERA
FIGURE 10.
FIGURE
FIGURE
FIGURE
FIGURE
11. DENDRITICSTATIC, STELLAR INDEX CAMERA 2i
12. FOG DUE TO LIGHT LEAKS, STELLAR-INDEX CAMERA. 2i
13. RESULT OF LIGHT LEAK, TERRAIN INDEX CAMERA -.2j
14. EXAMPLE Or- GOOD QUALITY, TERRAIN INDEX
CAMERA . 2k -
FIGURE 15. BINARY DATA BLOCK TRACKS INTO THE FORMAT,
FREQUENCY MARKS REFLECTED INTO THE FORMAT 21
FIGURE 16. MINUS DENSITY COMET AND LONGITUDINAL,
EMULSION SCRATCHES 4a
MINUS DENSITY, SUSPECTED CRIMP 4b
FIGURE
-FIGURE
FIGURE
FIGURE
FIGURE
17.
18.
19.
20.
21.
FIGURE
MINUS DENSITY THAT IS REPETITIVE 0.8" FROM THE
FREQUENCY MARK EDGE 4b
HEAVY INDUSTRIAL SMOKE, AND SOOT ON SNOW 6a
DEGRADATION DUE TO INDUSTRIAL HAZE 6b
PROGRESSION OF QUALITY ASSOCIATED:WITH -
CAMERA START-UP 6c
22. COMPARISON OF SMEAR ASSOCIATED WITH CAMERA
START-UP .6d
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LIST OF ILLUSTRATIONS (Continued)
FIGURE 93. PLUS DENSITY STREAKING ADJACENT TO CLOUDS- 6e
FIGURE 94. EFFECTS OF SUN AZIMUTH 6f
FIGURE 25. EFFECTS OF SUN AZIMUTH 6g
FIGURE 26. PHOTOGRAPHY AT NORTHERNMOST LATITUDE 6h
FIGURE 97. DISTORTION COMPARISON 8a
FIGURE 28. MISSION INFORMATION POTENTIAL (MIP) FRAME 8b
FIGURE 79. MIP AREA, FWD CAMERA 8b
FIGURE 30. GOOD QUALITY, SNOW COVER? 8c
FIGURE 31. COMPARISON OF IMAGERY 8d
FIGURE 39. PORTABLE RESOLUTION TARGET 8e
FIGURE 33. EDGE SPREAD TARGET 98a
FIGURE 34. PLOTTABLE PHOTOGRAPHIC COVERAGE 31
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SYNOPSIS
Mission 1004-2 (system J - 5 ) was the second
payload recovered from vehicle No 1174. The
first photography exposed on this Mission was on
pass D49 after ejection of the "A Bucket" (Mis-
sion 1004-1). Mission 1004-2 accomplished 64
revolutions of which 32 were operational (pho-
tography was accomplished). The payload con-
sisted of 5,858 panoramic frames (2,909 FWD,
2,949 AFT). Seventy-five feet of stellar index
film and 135' of film exposed in the terrain in-
dex camera was recovered. The characteristics
of the photographic take in regard to the pano-
ramic cameras is very similar to that of Mis-
sion 1004-1, which is considered to be a good
mission.
The panoramic cameras used on this mis-
sion operated well with the exception of soft-
spots on the master take and a few other minor
degradations.
Due to the large difference in densities re-
corded within a pass, portions of 19 passes of
the master and 25 passes of the slave panoramic
camera positives were reprinted at a Special
density for the Pl's.
The weather was eXceptionally good during
?this Mission, with only 32.5% cloud cover. An-
other factor that lends to the favorable overall
average of the mission .is that exposures were
generally glade while the solar elevation was
favorable.
The stellar index camera operated poorly
throughout the mission. When functioning cor-
rectly, stars to the fifth magnitude could be dis-
cerned.
The--terrain index camera functioned well.
The horizon cameras generally Operated
well but the port horizon appeared to be con-
sistently underexposed.
GENERAL FLIGHT DATA
Date of Launch: 15 February 1964
.Orbital Parameters: ?
Planned Actual (fZeNolution 92)
Period: 90.07 rain
Perigee: 100.0 nm
Perigee Latitude: (Not Available)
Apogee: 236.0 nm
Eccentricity: 0.019
Inclination An,le:. 75'
90.7 rain
102..3S nm
43.25' north
245.51 nm
0.019'
75.06'
PART I. CAMERA OPERATION
1. Master (FWD) Panoramic Carnera No 124:
This is the same camera used in Mission 1004-1_
Therefore, as would be expected, the character-
istics of the photographic take are very similar:
The photography is highly degraded, due to
image softness, in an area approximately 1.0':
wide along the camera number edge in the first
3 to 15 frames of nearly every pass. This soft
imagery extends from 3.0" to 8.0" from the
take-up end of the affected frames. There are
three small emulsion digs just inside the format
adjacent to the carnera number on every frame.
A minor Emulsion abrasion extends edge to edge
in line with each dig.
Minor corona static discharges and occa-
sional minor associated equipment shadow--
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often underexposed due to the unfavorable solar
elevations. Horizon imagery in all four cameras
is slightly vignetted but the vignetting does not
hinder the useability of the horizon arcs for ve-
hicle attitude determination. The design of the
horizon cameras now employed is-such that slight
imagery vignetting, will always be present.
5. Stellar Index Camera No D42/42/37: The-
camera operated erratically throughout the mis-
sion. There were eight double exposures during
the course of .the mission and 37 frames were
grossly overexposed and unusable due to the
shutter hanging open. The shutter als0 remained
open while the film was being advanced on 53
'occasions. Due to the shutter notOpening or not
opening long enough to form an image, 25 frames
are clear in the first 350 programmed. There
were no stellar images after frame 350. The
program called for 407 fraines. Thecorrelation
fiducial lamps did not function during the mis-
sion. Edge static is continuous on both edges
throughout. A diagonal plus density band, at-
tributed to a light leak, is apparent on nearly
every frame. The moon is imaged on frames
298-355.
6: Terrain Index Camera No D42/42/37: The
camera operated normally throughout the mis-
sion with the exception of a double exposure on
frame 5. The imagery recorded is of good quality
except for 8 frames affected by.a minor light
leak.
7. Collateral Equipment:
a. The 200 cycles per second (cPs) fre-
quency marks are present on all frames through-
out the mission. On the Master (FWD)cameras,
the marks are imaged in the format and, being
superimposed on the terrain imagery, are not
NPIC/TP-17/64
readable except on engineering passes and
passes where the imagery is of low density. The
frequency marks are printed outside Of the ter-
rain format on the slave panoramic camera but
are reflected into the format edge. However,
they are readable throughout and the reflection
does not seriously degrade the pan camera
imagery.
b. Li gh t number 11 Of the binary data block
on the slave camera did not function during the
mission. Light number 14 failed on frame 92 of
pass D85 and on all subsequent frames. The
binary data block of the slave camera tracks into
the panoramic format on most frames. The
binary data block of the master camera was
operational .and readable throughout except on
pas D72, frame 54; D85, frame 75; D87, frame
136; D103, franies 5.7 and- 103. The images of
the data block on . both cameras is slightly
bloomed.
c. The terrain and stellar index camera
correlation fiducial .marks failed to operate
during the entire mission.
d: The camera-off marker of the slave
camera recorded satisfactorily through pass
D56. On passes A56E, A71E and A72E it is .
superimposed on the binary word. The camera-
off marker of the master camera recorded satis-
factorily throughout pass D55.. The mark is
superimposed on the. binary word in passes
A55E, A56E and A71E. On all. passes after ?
A71E, the end-of-pass marker is misplaced and
usually appears over the first frame of the
'following pass.
e. The camera numbers, although bloom-
ed, are recorded and readable throughout.
PART II. FILM
1. Film Processing: This section provides a
descriptive evaluation of the exposure and the
processing, and comments on the exposure, the
density, the processing and the physical condi-
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tion of the original negative.
'Pertinent data was collected during various
phases of the processing and more thoroughly.
during the evaluation of the negatives. This.is a
standard procedure. The community is informed
by cable of any extensive defects in the photog-
raph' which . may affect the PI suitability of
any mission.
Support organizations provided the Pro-
cessing center with pre-launch samples of the
actual film used on this mission. These samples,
along with fresh process control stock, Were
sensitornetrically exposed and processed at con-
trolled levels of development. A characteristic
curve was prepared from these sensitometric
strips and is defined as the "Mission Material
Processing Curve."
? While the film was being prepared for pro-
cessing, it was inspected for physical damage
which could cause processing difficulties. -Dur-
ing processing, data was recorded giving the
processing conditions and film footage locations
where processing changes occur. Changes in
the normal course of processing which may af-
fect the film quality were recorded and, after
processing, the original negatives were examin-
ed frame by frame for defects and damage.
Most of the film on this mission received
adequate exposure. The solar elevation varied
from a low of -55? on engineering passes A103E
and A104E and -5? on operational pass D66 to a
high of 68? on pass D103. Acceptable photog-
raphy was accomplished with a minimum solar
elevation of approximately 4?47' in pass D67,
at- a latitude of 71'30' ribrth. The local time at
which the exposure was made was 0942. The
photographs taken. at the lower latitudes, where
the sun was relatively high (30?- 40?), tend to be
slightly overexposed. The greatest variation of.
density that is directly attributed to exposure is
in the horizon images. On the majority of frames
from both FWD and AFT panoramic carneras the
port horizons did not have optimum exposure.
lhe starboard horizons were properly exposed
rendering adequa{e density throughout most of
the mission.
The exposure of the stellar index camera
appears to be near optirnurn where not degraded
by the various shutter problems. The exposure
of the terrain index camera also appears to have
been near optimum.
Approximately 50 of the film exposed in
the pan cameras received intermediate develop-
ment, 13T, full, and 37;76 primary. Because of
exposure changes dueato variations-in sun eleva-
tion and terrain, approximately 50 changes in the
development level were made during -the pro-
cessing Of the slaile film and approximately 65
changes during the processing of the master film.
The gross fog density readings range from a
minimum of 0.07 to a maximum of 0.21.
The film from both the stellar and terrain
index cameras was processed normally.
The density of the pan camera photography
is near oprimurn considering the latitude.of ter-,
rain reflectivities encountered on the mission.
2. Film Degradations: This section lists some
of,the more notable film degradations and a few
frames on which examples of each can be found.
a. Master (FWD) Panorarnic Camera:
Corona corona discharges are en ident
in the horizon format of several
frames after pass D49. (Example:
pass DO, frames 1. 2, 20.) Minor
corona bursts are also common on the
third frame after a camera-on posi-'
tion. Examples of this may be found
on- pas,-- AT1E, and DTs. On
pass D64 and on all subsequent pass-
es corona .dischares become more
frequent and appear at inter\_als of
approximately G.:1". (Example: D64,
frame d.)
.\ diagonal band of plus density re-
alt no -from a lioht leak appears on
tie fourth frame of each p- ss The
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film suspended in the camera during
a camera-off position often is slight-
ly fogged, depending on the duration
of the camera-off period and the solar
eleNation during the period. (Ex-
ample: pass D94, frame 1.)
Manufacturing
Splice-
NPIC/TP-17/64
tam n fogging and equipment images
due to light leaks within the system.
(Example: pass A104E.)
Pass D35, frame 33: pass D71, frame
110.
Emulsion Digs
Four small emulsion digs are present
adjacent to the Camera number just
inside the format at each edge.'
Minus Density
.Comets
Appear at random throughout the mis-
sion. (Example: D71, frame 36.) -
Minus Density
Streaks ?
Dendritic Static
Manufacturing
Splices
Minus Density
Comets
Emulsion
Scratches
Faint minus density streaks appear -
on frames 2-22 of pass D67.
Small, minor discharges are present
occasionally in the third frame fol-
lowing a camera-on position. (EX-
ample: ,-72E, frame 3.)
Emulsion
Scratches
Rail scratches are continuous and
severe. Longitudi.nal emulsion
scratches appear intermittently
throu4diout the mission, and on pass
D49, Mission 1004-1.
Pass D49, frame 15: pass. D65. frame ?
167: pass D102, frame 57.
?
EXC('SSiVe and pronounced throughout
the mission. (Examples: D71, frame
36.)
Creases and
Tears
Rail
scratches are severe and con- .
tinuous. Several short, longitudinal -
emulsion scratches appear Within a
band edge to edge beginning ap-
proximately 3.0'' from the take-up end.
of 'each frame. (Example: D62, frau-le-
is.) Pass D111, frames. 26-2.ti were
severely scratched as loose film was
drawn through the camera.
Blisters and
Pinholes
Minor and Intermittent.
Severe creasing, tearing, etc., oc-
curred on Pass D49, Mission 1004-1
.at the processing site to such an ex-
tent that small pieces of film- were
completely destroyed. A series of
crimps and. creases appear on pass
0103, frames 96-95.* Severe film
damage occurred on the last 3 frames
of pass D11:2 ,as the loose end of
film was .drawn .through the camera.
Blisters
Some of the ,aforementioned minus
density comets were definitely the
result of blisters. They are moderate
in number but serious in nature.
Image Smearing
This is' common on the first 6 frame's
of most passes on frames exposed
before the system overcame inertia.
(Example: D62, frames 1-6.)
b. Slave (AFT) Panoramic Camera:
Corona Static
Light Leaks
Pinholes
Minor and intermittent except on pass
D71 Where th9v- are numerous and as-
sociated ? with the manufacturing
splice on frame 110.
There is usually a small discharge on
the third frame :ifter a camera-on po-
sition. (Example: D64_, frame 3.)
Pass DOG contains random discharges
throughout.
There is a plus density band caused
by a Ii gut -leak- on the fourth frame
after each camera-ron position. Sex-
oral patterns of fog are present on
pass D49 (Mission 1004-1). This ap-
parently is :issociated v.ith the cut
and wrap operation. The first and
last few frames of most passes con-.
A .minus density spot 'approximately
0115" in diameter appears intermit-
tently 0.5'' from the frequency mark
edge on pas DS6. frame 7 and On
,most subsequent frames. .Another
minus- density pattern, in the shape
of a? half-moon with a -tail projected
front its concave 'surface, also begins
on pass D56, frhme 7 and appears in-
termittently throughout the remainder
of the mission. The' spot is approxi-
mately 0.1" by 0.1- at the extremes
and a small- plus density is often not-
ed in the center of the half-moon area.
The pattern jt suggestive of a crimp.
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c. Stellar Index Camera:
Edge Static
Light Leak
. Terrain Index Camera:
Corona and dendritic static discharges
along both edges are continuous.
There are random static discharges
within the format.
A diagonal band of fog appears on
nearly 0'. en frame and is ?ery dis-
tinct on 2:2 frames.
Corona
Light Leaks
Static discharges are continuous along
both edges.
Frame 16 only.
.A band of fog projects into thit format
from the camera number edge of frames
19, 21, 29, 4ti, 49, 67,?74 and Sl.
PART III. IMAGE QUALITY
1. Photographic Interpretation (PI)Suitability:
This is an assessment of the information content
of photographic reconnaissance material and its
interpretability. A number of interrelated fac-
tors are involved, such as the quality of the pho-
tography, the -extent of target coverage, scale,
weather limitations, and similar considerations.
However, the fundamental criteria for assigning
a PI suitability rating may be reduced to (a) the
scope of the photographic coverage and (b) the
degree to which a photo interpreter may extract
useful and reliable information from the
material.
PI suitability ratings are categorized as
Excellent, Good, Fair, Poor, and Unusable.
These ratings refer to the overall interpretive
value of the photography obtained from a particu-
lar reconnaissance mission. Individual targets
may also be assigned PI suitability ratings if
that is necessary or desirable. The standards
?that determine assignment of the various ratings
are as follows:
Excellent: The photography is free of de-
gradation by camera malfunctions or processing
faults and weather conditions are favorable
throughout. The imagery contains sharp, well-
defined edges and corners with no unusual dis-
tortions. Contrast is optimal and shadow de-
tails, as well as details in the highlight areas,
are readily detectable. Observation of small
_
objects and a high order of mensuration are
madeopossible by the consistently good quality
of the photography.
.
Good: The photography is relatively free
of degradation or limiting atmospheric condi-
tions. Edges and-corners are well-defined. No
unusual distortions are present. Detection and
accurate mensuration of small objects are feas-
ible, but to a lesser degree than in material
rated as "Excellent".
Fair: Degradation is minimal but the acuity
of the photography is less than optimum. Edges
and corners are not crisply defined and there is
loss of detail in shadow and/or highlight areas.
Detection and identification of small objects are
possible but accuracy of mensuration is reduced
by .the fall-off in image quality and the less-
than-optimal contrast that prevails.
Poor: Camera-induced degradations and/or
weather limitations severely reduce the ef-
fectiveness. of the photography. Definition of
edges and corners is not sharp. Only gross
terrain features and culture may be detected or
identified and distortion of form may exist.
Accurate mensuration of even large objects
is doubtful.
Unusable: Degradation of photography com-
pletely precludes detection, identification and
mensuration of cultural details.
2. PI Suitability for Mission 1004-2: The PI
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suitability for this mission is considered to be
good in that fine detail is readily discernible.
through most of the mission. Photo interpreters
reported on 140 targets in the preliminary tar-
get read-out of which 95-', were given quality
ratings of poor and the remainder a rating of
good. Snow was the degrading factor on 657, of
the targets receiving poor ratings while haze was
to blame for the remaining 35-c. Highlights of
the mission coverage are as follows:.
a. Discovery of construction and activity
observed at a missile test center.
b. Discovery of construction at a nuclear
weapons proving ground.
c. Clear count of aircraft at a military
airfield.
d. Identification of a radar array.
e. Discovery of a large area of new con-
struction.
Mission 1004-2 produced imagery only
slightly inferior to the best ever attained by. the
KH- 4 system. The degradations that are present
and the problems encountered that have a direct
-bearing on PI suitability are as follows:
Corona Static - The degradation of imagery
due to the effects of corona discharge is minor
on both panoramic cameras.
Light Leaks - Diagonal patterns and equip-
ment shadowgraphs are usually present on one
or more of the first five frames and on the last
three frames of each pass on both the master'
and Slave .panoramic cameras. The fog caused
by the light leaks is minor but it does have a
degrading effect. A good example of the various
fog patterns may be observed on- pass D64,
frames 4 and 5. These light leaks are- a result
of the -camera design and are not an anomaly.
Scratches and Abrasions -- Four small
emulsion digs at each edge of the format, adja-
cent to the camera number, appear on most
frames of the master camera. Although these
digs are small, had a target fallen in this area,
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it would have been degraded or lost. -
Atmospherics - 32.657, of the photographic
take of this mission is obscured by clouds..
Eighty-two known targets were not reported
due to atmospherics. Haze degraded 5 targets
,to such an extent as to be rated poor for pho-
tographic interpretation'.
Solar Elevation - Most photography was ac-
complished while the solar elevation was favor-
able and little imagery was lost.
Image Motion - The first few frames after
each camera-on position display this condition.
The slow camera speed at the beginning of pass
becomes more pronounced as the mission pro-
gresses. The PI suitability is highly degraded
on the affected frames.
Minus Density Comets - While each comet
is very sfnall, the large number of them en-
coiintered on this mission makes them a de-
grading factor.
Minus Density Spots - The small minus
density spots on the take of the slave camera
Suspected to be roller-induced crimps would
obscure any imagery within their path.
Soft Spots - The imagery within the area
described as being of "soft focus" on the master
camera is highly degraded and of little use to
the :pi .
The image distortions inherent in the KH-4
camera are common throughout the mission.
Pass D62, frames 17 FWD and 22 AFTare good
examples.
Plus and minus density streaks associated
with areas of heavy density (clouds) are noted
intermittently throughout the mission.
3. Mission Information Potential (MIP): The
MIP is an arbitrary nuriaber, not limited by
terminal values, which is subjectively assigned
to the Panoramic photography of a mission and
which compares it to the other KH missions. It
is meant to be a measure of the camera's maxi-
mum capability for recording information, dis-
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counting adverse atmospheric conditions, mini-
mal solar elevations, camera malfunctions or
other factors which reduce the quality of the pho-
tography. The NIIP is based on the best photog-
raphy found in a mission, even though the pho-
tography may be limited to a few frames. Since?
these frames are considered the best in the miS-
sion, they do not indicate the overall success,
average quality, or general interpretability of
the photography.
Criteria for selection of an MIP frame:
a. Eliminate all portions of the mis-
sion affected by system malfunctionS.
b. Select frames which are free of
clouds and atmospheric attenuation.'
c. Eliminate the first ten frames sand
last frame of a pass as these may be af-
fected by incorrect scan speed.
d. Select frames that are in a con-
tinuous- strip of approximately ten cloud-
free frames, as cloud shadows from distant
weather fronts are cast for great distances.
e. Determine from the horizon cam-
eras that the panoramic photography is not
affected by apparent vehicle perturbations.
f. Select targets that are near the
? center of format and on frames as close as
possible, to perigee for scale purposes and
to eliminate obliquity.
g. Select frames having near optimum
solar elevation, thus eliminating frames
having either overexposure or underex-
? pos ure.
? h. -Select a high contra-st target (pre-
ferably an airfield) and compare the target
to a previous mission which has been given
an MIP rating.
4. NIIP For Mission 1004-2: Utilizing the
criteria set forth in the preceding items, pass
D62, frame 23 AFT was selected as the MIP
frame for this mission. The mission was given
an MIP rating of 85 and is comparable to Mission
1004-1 (also MIP 85).
The photographic scene covers a city and
airfield which are located near the center of the
format. Image quality is such that runway mark-
ins; aircraft engine nacelles (on larger air-
craft), and vehicles in parking lots and on high-
ways are discernible.
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
Next 4 Page(s) In Docu2nliirit Exempt
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
TOP SECRET RUFF
NO FOREIGN CISSEM
NPIC/TP-17/64
,
Pa;,oramic Can; eras
APPENDIX A. SYSTEM SPECIFICATIONS
Stellar oh,2 Terrain, Iiidc-r Cameras
\faster
(F?% D)
Sl as
(AFT)
Stellar
Terrain
Camera No . 124 125
Lens Serial No 0642435 .1022435
Slit 11idth 0.250y 0.250"
Aperture f 3.5 f ?3.5
Filter ?Nratten 21 1Nratten 21
Operational Focal Len!rth 609.60 mm 609.60 mm
Film Type 4404 4404 '
Film Length 7500' 7500'
Emulsion 45-73-12-3 45-73-12-3
Static Bench Test .
High Contrast 290 L mm 235 L 'rnm
LOW Contrast
Dynamic Test
I. High Contktst
I. LOW Contrast
P. High Contrast
P. Loss Contrast
160 L mm 155.L "mm
170L .rnm
. 131 L mm
1.53 L..mm
107 L..mm
175 L "rnm
*135 L mnL
215 L 't-nrn
-105 L 'rnm
Camera No
Lens Serial No
Reseau Serial No
Filter
Aperture
Exposure Time- -
Operational Focal
Length
Film Type
Film Length
Splices
Emulsion
Perpendicularity of
Reseau
-Location of Principal
Point
.Awar
D42-'42."37
10510
None
f WS-
:2 sec
NA
D4-2 '42.'37
S13050
42
1Vratten 21
fr 4.5
1.'500 sec
NA
4401.. ;1400
75' 135'
None None
.7-3-1-4 16-4-11-3
0.00-0.93" 0.00"-2.25"
Panoramic Camera No
Lens Serial No
Exposure Time
Aperture
Filter
Operational Focal
Length
Average Lines mm
?Radial Resolution (L/mm)
lOs off axis .
20' off axis
Tangential Distortion
Starboard
(Take-up)
124
812265
1 100 sec
1. 5.0 ?
ISratten 25
54.45 mm
162 L .trim
.009 mm
.012 mm
.004 mm
Port
(Supply)
Starboard
(Supply)
124
812271
? 1.'100 sec
f -
{1ratten 25
54.33 mm
1:25
51227q
1:100 sec
f,"5.0
Wratten 25
55.45 mm
-,015 mm
-.015 mm
Not AVailable
.004 mm
.002 mm
.005 mm
- Port
(Take-up)
125
512272
1.'100 sec
f 6.5
1\ ratten 25
5f,.45 mm
178 1...rnm
.002 mm
.009 mm
.003 mm
Camera:No 12..:
Resolution Take-up
Angle Off Axis
Radial Resolution (L/mm)
Tangential Resolution (L/mm)
10?
141
141
Supply
0'
157
177
10? ?
141
141
20' -
106
SS
Resolution
Angle Off Axis
Radial Resolution (L/mm)
Tangential Resolution (L/nim)
Resolution
0?-
154
164
164
145
10'
144
142
Camera 'so 1L'5
Take-up Supply
15?
112
115
20?
103
56
?5?
105
CO
0'
164
164
5'?
164
162
10'
162
151
15?-
134
121
20?
109
91
27.5?
41
41..
Stellar Index
Angle Off Axis
High Contrast
Low Contrast
NA
NA
NA
NA
NA
NA
NA
NA
N.A
NA
NA
NA
10?
92
53
20?
" 108
91
30?
59
pp rove
? ''' ' ",ft
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
Slave(All)Caniera
Serial No 125,
Stellar Index B
Serial No D42'42/31
? Retro Rocket
Stellar Index A
Serial No D29'29 29
Master( Fwd)Camera
Serial No 124
,z7ro.Y.F4P7w,P47,77-'5'
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
FILM SPECIFICATIONS
FORMAT LAYOUT
Format No 1
(No Horizon Format)
? Format No 2
(2 Horizon Formats)
' Clock Interrogate
(Missing Pulse)
Format No 3 ( No Horizon Format)
Horizon Format
for No 2 Format
Supply Side
(Records Every Other Cycle)
? Stellar Inde
Operation
' (Stretched Pulse Every 7th Frame
Master Camera Format Only)
1/3 Format Mark
Camera Serial No
Horizon Format For No 2.
Format Take-Up Side
(Records every other Cycle)
Master(Fwd)Panorainic Camera No 124
Viewed With Negative Emulsion Down
Direction of Film Transport
Direction of Scan
Direction of Vehicle Motion
Slave(Af0Panoramic Camera No ? 125
Viewed With Negative Emulsion Downs
Direction of Film Transport
Direction of Scan ?0?
Direction of Vehicle Motion
?
151114,,,-.11114171-417,471'1',14441.14,..
,
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0'
FILM SPECIFICATIONS
FORMAT SPECIFICATIONS
. Viewed with Negative Emulsion Down
"4-- (Jinx.
XVO
Master (Fwil)Caniera . Vehicle Motion Scan Direction
76.1 Xt ' i 0.225 Dtx +0.226
355.3 Yl -0.089 Dty 42.0/0
710.3 . Xs -0.393 Dsx 0.394 '
56.496 Ys +0.036 . Dsy 2.000
- 56.435 Xvo '0.757 Dam +0.773 --
Yvo r1.104 DfilY 2.000
Format dimensions:
Panoramic Take-Dp ? Supply
Height ? 55.9
Width ? 756.4
Vehicle Motion
Scan Direction
76.1 Xt 0.045 Dtx -0:047
B 355.3
C 710.3
56.488 Ys 10.045
56.459
0SY 2.000
? Xvo -0.737 Dine -0.749
Yvo +0.306 Dmy -2.000
Format dimensions:
Panoramic Take-Up Supply
Height 56.2
Width 755.3 ?
NOTE: 1. All dimensions are in millimeters and are average dimensions of three formats
2. Height of main format is taken at center of format
3. Dt, Dm, Ds, X and y dimensions are taken 10 WA above point defining target center
4. Format Sign Convention
?X+Y +X+Y
+X?Y
ii c J?0492 In '1141
lag IMO MO NS IN SO MS 041 ME MI M WM ,1119
64%-a..cf
TOP SECRET RUFF
NO FOREIGN CISSEM
APPENDIX B. TECHNICAL COMPENDIUM
-
Terrain
Lin0ting _
? i
Fr 'o
0,er-?
(110u(1
U''''
S'-1'
:-'11iiir
rit(?11
11011
( AII
-AIL
D
D
1
D
D
A
Fog
Exp
lap
Ti""
-ri,-.:,-
El.,.
minu,r
(.I5-)
Min
Max
\lin
Max
D19 . 01 NI: 2321 ...2309 11107 51'43 NA- NA NA NA NI: NR NI; 0.37 2.25 1.,, 0.11 NA
D00 05 00 4212 0110 1027 -0, 21 14554 -00=07' t(1=05 244719 0.71 1.69 0.95 0.74 2.05 1.31 0.01 1 211 -
DO o 11 07 41111 ' 011, 1110 11 :90 15011 00 12 01 04 11227110 0.51 1.34 0.93 0.51 1.92 1.41 0.11 1 2.0
D02 0, 00 1111 0424 1220 :11 01 10 10 0)115 01 42 2117,2 0.62 1.21 0.59 0.42 2.05 1.63 0.11 1. 206
D02 ,(1 07 1111 0420 1029 :15 39 11 00. (0)25 01 20 20,772 1.25 1.9, 0.73. (0,5 2.13 1.2, 0.11 1 1257
D:43 07 1111 (1500 1117 21 i,5 15:19 00 07 01 01) 223709 0.,9 1.95 1.06 00,7 2.06 1.19 0.21 1 23,
D53 57 09 1111 0006 10:12 36 4, 15 (If (0:16 NA 20714, 0.9, 1.99 1.01 0.9, 1.99 1.01 0.11 1 257
'D54 02 ,,,) 2,2,1.1 ,(71!1 1027 ()=. 30 14 47- 00 :!:1 01 07 04795" 0.27 o.4-r 0.17 0.07 0.07 1.550 (600. 1.19-1
i D.54 - 75 00 .1111 072:1 1147 21 50 15 20. (0(53 01 55 2227:13 1.07 -1.67 0.00 0.60 1.74 1.14 0.0, 1 "241
054 ,7 (a; 1111 0721 1155 2:1 14 10.20 00 01' 01 39 21(0)02 0.s3 1.51 0.6, 0.06 1.05 (1.99 0.0, 1. 245
- D54 102 NI: 1111 07110 1004- 25 49 15 15 0)45 NA 217002 1.35 1.59 0.24 0.00 1.71 1.11 0.0,_ 1 .247
D55 00 Niz 5555 00,49 100 05 :1, Ii 52 -0,/ 17 00 1, 2536011 Nil NR NIZ (634 1.63 1.29 0.16 1 '156
DOS 05 01 3115 0,50 15,05 00 02 14 S -0(19 00 1, 246016 NR Nil NR 0.22 1.,5 .1.52 0.20 1 '206
DOS.4 NR- 5555 0,5:1 11:16 1, 2:1 14 0, 00 10 01 02 207902 NI: NR NIZ' 0.7, 1.30 0.511 0.07 1 .237.
DOS 124 i 00 1111 0,50 1-159 2407 15 12 01110 01 14 -21914, (075 1.55 0..50 0.75 1.63 0.,., 0.07_1;245.
1300 10!) 0, 1111 00.00 1215 :10 01 15 54 00 15 01 09 214201 1.3, 1.'50 0.42 (),3 1.,0 0.97 0.0, 1. 203
DOS 20, 00 1211 0900 .1211 4:2 3" 11 24 00(10 00 57 205000 0.57 0.94 0:37 0.41 2.20 1.,9 0.0, 1 261
D50 00 0...,. 2111 1027 .1014 11950 150, (11( 07 01 11 21:1490 1.09 1.55 0.50 1.00 1.55 0115 (60, 1 255 .
D61 .N1Z 4450 1,01 *1210 NA 15:19 -00 17 00 02 2005,1 NR NR NI: 0.i-0 2.14 1.34 0.09 1 -25,
D00 01 00 1111 1930 .1311 4:2 5-1 1505 00(0. NA :200(gm 1.30 1.,2 0.52 1.30 2.00. 0.7, 0.09 -NA
D02 02 1/0 1111 19:11/ -1:110 111 00- 10 05 00 0, NA 20000(-9 0.62 1.3, 11.76 0.62 1.6, 1.00 1009 1 .11
11)(12 00 1111 1930 .1317 431'I 24 00 07 NA 201000 (040 1.69, 1.2, 0.40 1.6, 1.2, 0.09 1 224
D62 04 02 1111 19:10 131, 13 32 15 24 00 07 NA 204500 (04, 1.40 0.94 0.4, 1.72 1.24 0.11 1:240
11/00 . 05 04 1111 19:16 1319 43 40 15 113 00 OS NA 204000 0.6, 1.5, 0.90 0169, 1.,2 1.14 0.11 1..246
D02 06 0 ti 1111 1936 1319 13 40 150:1 00 OS NA 204500 0.72 1.4, 0.76 0.72 1.92 1.20 0.10 1 250
D02 17 02 1111 1937 1221 45 0f6. 15111 00 00 00 46 201500 0.60 1.70 1.0, 0.40 1.7, 1.3, 0.10 1 '25S
D02 1, 03 1111 1937 1321 ISO-. 15 00 0:1 (6)46 204550- 0.6, 1.90 1.22 0.6, 1.90 L22 0.11 1 :209
D04 11.0 0, 1111 112.0 10(0. .14 :14 -00 07 -NA 229420 0.60 1.62 1.02 0.50 1.,0 1.22 0.11 1 224
D64 60 07 2252 1450 00 0, 14 40 00 20 0036 275757 NI: Nit NI: (04, 2.21 1.73 0.11 1 19:2 .
11/00 1, 00 1111 2359 1049 11 30 10110 ((052 NA 23903, (661- 1.0, 0.97 (660 1.,4 1.24 (611 12119
D65 49 09 111-1- 0001 1101 16 47 15 13 00(1'. NA .227360 0.55 1.60 1.11 0.27 1.91 1.64 0.09 1 239
_ D66 ..... - 07 1111 0130 112, 19 20 14 3, 00(01 NA 2202119 0.02 1.73 ..119 0.27 2.03 1.76 (611 1 23.1
D00 04 0, 4313 013) 1140 24 11 15 37 00(0) 00 31 21,000 1.01 -2.13 -1.12 (653 2.14 1.61 0.11 1 246
D66 ? 74 16 4313 0134. 1151 20 21 IS :10- ((013 NA 247000 (),,2 1.92 1.10 . 0.6.6 2.22 .1.1(6 O1), 1..04, _
D(17 21 10 1111 0259 0910 (14 17 11 0, ((031 01 16 21,400 0..60. 0.90 0.22 0.46 1.32 0.S6 0.20 1 .214
D07 44 09 1111 0305 120:1 26 01 ISO, 00.23 ((045 215102 0.72 0.00 0.2, 0.61 2.06 1.40 0.20 1 .244
D0, 4, 09 1121 0135 1144 :1431; 11S3 00 03 NA 21,37, 0.60 1.91 1.3f 0.60 2.09 1.4, 0.11 I 100.
D6, - 63 1,0 1111 0430 1152 06 56 14 40 .0003 0020 215339 o.0, 1.6, 1.10 0.5, 1.94 1.36 0112 1 249 -
Df1, 132 10 1112 0139 1217 36 39 14 57 00 10 01 19 207000 (1.96 1.7, 0.92 0.S4 1.92 1.0, 0.10 1 '25,5
1 Di1, 101 00 2213 ((440 1220 40 45 11 54 0910 ((103 205000 NI: Nil Nil 0.39 2.03 1.64 0.11 1 z260_
D09 07 10 1111 0604 1120 1.5.'13 15 57 00 45 NA 227049 (054 1.66 1.12 0.54 1.96 1.42 0.11 NA
1:109 11 09 1111 0000 1120 23 29 15 52 (90(1 NA 217449 1.04 2.00 0.96 1.04 2.10 1.12 0-..21 NA
D70 09 09 1111 0730 1120 19 59 14 4, 9931 01 23 520921 0.76 1.,0 1.06 0.76 2.02 1.26 0.21 1 '23, ?
D70 97 0, 1211 0740 1210 3554 14 34 00 20 01 02 20733, 1.36 1.90 0.04 1.20 1.99 0.7, 0.09 0 '259
D71 0, 07 1114 0900 1101 1, 05 14 56 OD 01 NA 224730 0.94 1.42 0.4, (0,0 1.10. 0.,, 0111 _1 .237
1)72 22 12 11121 1029 1112 0401 iS 1, -00 10 00 3' 210000 Nil NI; 0.26 2.04 1.7, 0.11 1 247
? D72 10 11 1111 1010 1155 27 50 15:14 -00 05 NA 213000 1.00 1.93 0.93 0.72 0.07 1.25 0.09 I 251.
D72 74 10 1112 1045 1220 41; 39 10 04 00 0, NA 005230 0.6.9 1.92. 1.22 0.65 0.19 1.54 0.21 1 .259
D70 ,4 11 1111 1010 1241 4, 1, i16 01 On 19 01 0, 205000 1.10 1.70 0.60 1.10 2.00 0.90 0.1, I ',59
D7, 00 10 1111 1917 1211) 117-00 15 11 00 01 00 43 2065110 NH NR NR 1.16 1.96 0.s0 0.10 1 :24,
D7, i5 11 1111 191, 1217 111:1 15 17 .0.10'. NA 005500 .1.I, . 1.44 0.20 0.52 1.90 1.39 0.09 1 255.
D,2 III 01 1 1 1 1 1511'. 1133 05 :1:1 15 11 00 12 00:11 215000 0.96 1.96 100 0.70 1.9, 1.2, (611 1 .247
D,2 42 - li 2111 0:1111 11:51 3130 14 50 no 19 NA 2110(10 1.1, 1.91 0.60. 1.1, 2.02 n.,,--; 0.0., 1 :254
D,3 .7f; 10 1211 0320 1.007 :10 111 11 51 00 2:1 10 4'. 207-700 0.74 1.92 1.19 0.3, 2.02 1.64 0.11 1. '257
D,5 11 1111 001, 1120 21 14 15 -,,,, 01 NA 21,902 0.94 1.97 1M3 0609 2.06 1.37 0.19 1 1142
TOP SECRET RUFF
NO FOREIGN DISSRM
'` '
TOP SECRET RUFF
NO FOREIGN DISSEm
NPIC/TP-17/64
-Terrain
Limiting
..
YaW
I
Pu,
Frame
User
Cloud
1.105-
SI-I(1
Solar
Pitch
. Roll
(All
Ait.
D
D
A
D
D
Fog
A
Exp
lap
Tir,,,
Time
Lies.
Minus)
(Ixis)
Min
Max
Min
Max
D'.5
D05
D66
Ds6
D57
D57
D94
D94
D34
D114
D101
D101
D102
D103
D103
D103
D103
D103
D103
DIII
51
03
75,
93
45
1,4
01
02
16
Ils
-10
42
92
11
30-
137
150
169
10
10
10
11
09
01)
11
09
00
00
05
00
00
10
09
11
11
II
On
10
10
11
0620
0622
o749
0752
07.53
0920
0923
2001
2001
2001
200:1
0632
0633
0s04
.0932
0933
0935
0942
0943
0944
2135
1141
1200
1121
1153
1200
1120
1150
1209
1209
1212
1215
1124.
1137
1159
1059
1115
1137
1227
1220
1232
0940
97 47
:17 37-
.2" 3'
34
24 (1()
34 39
44 05
14 05
46 03
49 11
26 00
30 32
31 36
19 29
23 44
31 02
60 49
61 24
63 45
07 11
15 26
14 53
15 45
14 59
15 17
15 04
15 15
14_56
14 57
15 05
15 11
is 26
15 17
15 27
15 10
15 32
15 15
14 19
14 26
14 36
14 53
00 24
00 09
00 22'
00 :12
00 2;
.-00 01
00 09
00 07
00 07
-00 02
-00 02
-00 02
00-20
00 06
-00 04
00 05
00 23
-00 04
-00 06
00 07
-00 17
*All yaw ?alues are determined from stellar readings.
N
NA
01 02
NA
00 30
NA
01 (11
NA
N .
? N-h
N
NA
NA
NA
NA
NA
N
NA
NA
21196
216060
209090
207000
-216976
207,,S0
205335
205335
2060(50
206000
212250
299336
20o6 1,5
210000
214500
209100
214500
216000
222000
230500
(1.-12
0.05
0..S5
1.19
0.60
1.10
1.40
0.72
0.70
0.0)
0.00
0.95
1.09
0.57
0.44
0.53
1.03
0.01
0.00
0.47
0.05
1.74 1.32
1.91 1.06
1.07 0.99
1.75 0.26
1.72 0.64
1.96 0.76
1.04 0.36
1.72 1.00
1.64 0.56
1.70 0.90
1.64 ().04
1.50 c'-0.55
1.59 0.50
1.49 0.6'
_175 1.21
1.05 1.3''
1.66 0.65
1.33 0.5'
1.51 0.71
1:44 0.97
0.95 0.10
Note NR denotes no readint. made
NA rcienotet not axailable
.0.41
0.69
0.56.
1.01
0.5.0
1.10
1.40
0.64
0.70
0.70
0.40
0.95
1.09
11.56
0.37
0.51
0.61
0.34
0.35
0.20
0.77
2.00
2.0::
1.67
1.72
1.90
2.0,
1.92
1.76
1.50
1.00
1.70
1.62
1.77
1.95
2.03
1.50
1.52
1.94
105
1.44
147
1.31
1.17
0.56
0.04
0.00
0.60
1.25
0.90
0.00
1.40
0.05
0.73
1.21
1.50
1.52
0.99
1.40
.1:59
1.65
0.67
0.11
0.09
0.09
0.09
0,07
0.11
0.05
0.11
0.10
0.10
0.10
0.07
0.07
0_09
0.09
0.09
0.07
0.07
0.07
0.07
0.19
1 '251
1 "253
1.246
1 '255
1 '254
1.'247
1:256
_NA
1 '192
1 '249
1 '254
1;247
1.'254
1.'259
1,-249
1.255
1.'260
1236
1.246
1:246
1.236
Terrain
Limiting
D Max Raro(e
D (din flange
Aserage D Max
.-'erase D Min
0.44-2.13
0.27-149
- 1.66
0.53
D Max Range
D Min 'Tariff,.
As erase D Matv
.Average D Min
1.30-2.20
0.20-1:40
1.90
0.67
Gross Fo,, flange 0.07-0.21
At erase Gross Fog (1.11
2. Slaz.c 1.-1FT) l'araoramie Camera
_
-
Terrain
limiting
Pass
Frame
"9
Over-
I ap
Cloud
,
Univ.
Time
Sun
Tit:ie
solar
Elev.
Pitch
(All
,,,,_ v
....us(
Roll-
-
Yaw
(All
Minus)*
Alt.
(Yds)
D
Min
D
Max
A
D
Min
D
Sfax
A
Fog
Exp
49
D49
D5(1
D.50
D52
D52
D53
1352
D5-1
054
D51
D54
02
06
10 -
49
63
90
12
62
09
00
91
107
Nil
05
07
06
04
04
04
00
06
06
2359
2359
'0116
0110
0-124
0425
0552
0556
0719
0723
0724
0725
1307
1307
1029
1116
1220
1229
1147
122,
1027
1147
1155
1204
NA
5143
OS 21
14 36
31 51
35 39
21 25
36 45
05 26
211:,50
2:144
25 49
13'50' ? -00'10'
14 05 -00 07
15 00 00 12
14 52 00 1.
14 44 00 (25
15 00 , 00 35
14 OS 00 16
14 50 00 26
15 (17 00 23
14 26 0)) 53
14 20 00 51
14 29 00 45
NA
01'05'
01 04
01 42
01 25
01 ((0
NA
01 07
01 53
01 19
NA
NA
206360
244719
233726
211702
20077'
223759
207145
247955
222733
219022
21702'
0.67
NI)
0.64
0.75
1.11
1.41
0.79
1.23
0.49
1.24
0.75
(1.60
2.24
NR
1.23
1.61
1.74
2.21
1.92
1.97
0.75
1.07
1.52
160
1.57
NI)
0.59
0.0.6
0.63
0.50
1.13
0.74
0.26
0.63
0.77
1.00
0.30
0.21
0.64
0.50
0.95
127
0.67
1.23
0.30
_1.24
0.75
0.49
2.25
2.25
2.06
1.79
2.17
2.04
1.97
0.S3
1.93
1.52
1.03
2.05
2.04
1.42
1.21
1.22
0.95
1.37
0.74
0.45
0.69
0.77
134
1 '240
1 .2-1S
I '214
1.:227
1 251
1 '254
1'255
1 '215
1 239
1 '242
1 '246
TOP SECRET RUFF
NO FOREIGN DIS5=M
TOP SECRET RUFF
NO FOREIGN DISSEM
NP IC/T.P.- 17/64
Terrain
Limiting
Frzii-ne
0?or-
lap
Cloud
Unix.
Time
Solar
? Yaw
(All
Minus).
Alt.
(yds)
aN
D55
D55
D55
D55
D55
D55
DIG
DIG
- D61
D62
D.62
D62
D62
D62
DG2
DUO
D62
D64
D64
D65
D65
D66
D66
D67
DtI7
Dt-35
DCs
D,.;8
ID;t3;-;"
Dt39
D70
D70
.D71
D72
D72
D72
D72
D78 ?
D78
D83
, D53.
D.53
DS5
DS5
11)5
Ds6
DS6
DSC
D67
D57
D94
D94
D94
13101
D101
D102
D103
D103
D102
0(4
10_
90
-12s
164
260
03
Cl
40
06
07
09
- 11
:22
23
? 41
65
24
54
69
79
26
50
54
69
125
167
12
46
14
101
14
25
79
s9
09
3()
15
45
50
16
56
55
so
95
50
59
07
22
43
15
47
97
16
42
91
Nil 5555 0549 1600 05035' 15 02
02 3445 0550 1005 06 02 14 56
NI? 5555 0553, 1136 15 23- 15 26
04 1111 0555 1.159 24 27 14 42
05 1111 0556 1215 30 01 14 00
07 1211 0900 -1244 42 35 15 20
02 1111 1025 1149 02 00 15 04
06 2111 1007 1214 29 52 14 46
-NI1 4455 1504 1310 NA 1424
03 1111 1926 1314 42 54 14 29
- 03. 1111 1936 1315 4306 14 29
04 1111 1926 1317 43 19 14 30
04 1111 -192g .1315 43 32 14 30
02 1111 1936 1319 43 40 14 31
02 1111 1937 1221 45 05 14 23
03 1111 1937 .1)321 45 05 14 22
05 1111 1937 1325 .46 45 14 16
07 1111 222s 1125 .10 OS 15 20
05 2222 2252 1450 60 25 15 14
06 1111 2359 1029 11 32 14-25.
05 1111 0001 1121 16 47 14 31
04 4313 0134 1145 24 11 14 32
OS 4313 0134 1151 25 21 14 31
06 1111 0259 0942 04 47 14 40
09 1111- 0205 1203 26 01 14 41
05 1121 6425 1144 24 26 15 11
09- 1111 0426 1152 -26 56 15 13
'08 _ 1112 0439 1217 26 29 14 55
07 2213 0440 1226 40 45 15 Or
06 1111 0604 1120 15 11 1403
09 1111 0606" 1122 '22 29 14 05
10 1111 0726 '1126 19 59 15 01
07 1211 0740 1215 25 54 15 23
07 1111 0906 1121 15 55 14 55
11 2121- 1029 1142 24 21 14 33
10 1111 1040 1155 27 55 14 20
10 1112 1045 1235 46 29 12,50
10 1111 1046 1241 45 IS 13 595
06 1111 1947 1210 27 05 14 46
05 1211 1945 1217 40 02 14 43
09 1141 031, 1133 25 33 14 45
10 2111 0319 1151 31 32 15 0S
09 1211 0320 1257 36 16 15 03
07 1111 0616 1120 21 44 14 12
09 1111 0620 1141 27 47 14 34
11 4312 0622 1226 37 37 14 57
05 4312 0749 1121 22 32 14 15 .
07 1111 0752 1153 32 17 14 49
OS 4412 0753 1200 34 46 14 35._
09 1111 0920 1126 24 00 14 52
05 4424 0923 1155 34 39 14 34
06 1111 2001 1209 44 05 14 53
07 1111 201/1 1212 4003 14 45
07 1111 2003 1215 49 11 14 43
OS 1111 0632 1124 26 O. 14 31
07 1112 0633 1.127 30 32.- 14 :37
NI? 1121 0,04 1159 21 36 14 25
10 5224 0922 1059 19 29 . 14 21 '
10 3111 0922 1115 2344. 14 21
10 1111 0935 11317 31 02:.. 14 39
*All. yr ,alues are determiner] from ,tellar reading-.
00 17 00 16
05) 19 00 15
00 10 01 02
00-10 01 -14
00 15 01 09
. 00 06 00 57
-00 06 00 42
00 07 01 11
-00 17 00 a:3
oo 08 NA
00 0, NA
00 07 NA
00 07- NA
00 05 NA
, 00 02 00 46
_010 03 00 46
00 06 NA
-00 07 01 25
00 20 00 36
00 03 NA
00 OS NA
00 04 00 31
00 19 NA "
00 25 01 16
00 42 00 45
-00 02 NA
-00 04 00 22
00 14 01 19
00 12- 01 03
00 45 NA
00 06 NA
00 31 61 23
00 24 " 01 62
00 01 NA
-00 10 00 32
-00 03 NA
00 11, NA
002s 01 OS
00 01 00 43
-00 OS NA
00 05 00 31
00 21 N.:1
00 21 06 45
-00-113 NA
00 24 NA
-00-01 NA
00 23 01 02"
00 31 = NA
00 25 00 35 -
00 00 NA
0008 01 01
- 00 07 NA
-00 01 NA
-00 01 NA
-00 04 NA
00 27 NA
00 04 NA
-00 02 NA
00 07 NA
00 24 ' NA
253602
246516
227902
0J9145
214201
20i1000
221745
213492
205551
205000
2 05000
204650
204500
204500
204550
204550
204600
229425
275757
239035
.227365
21:5000
217000
245400
Nil
NI?
Nil
1.40
1.20
0.55
0.27
1.09
NI?
0.70
0.71
0.56
0.52
0.72
0.65
1..12
0.50
().55
0.41
1.49
.1.41
1.23
0.37
215152 0.35
215375- 0560
215339 0.65
-207000 0.49
205550 0h60
22-7049 0.52
217449 0.50
222921 -0.55
207335 0.90
2.24730 0.63
216000 0.33
212000 0.93
205250 0.97
205000 1.21
206500 1.70
0205500 0.37
215000 1.33
211000 0.15
207702 0.49
216962 0.S0
211596 0.50
206562 0.91
216000 0.4.5
209000 1.71
207000 1.02
216976 0.75
207650 1.09
205335 0.72
206000 0.55
206000 .0.77
212250 1.05
209226 0.95
205655 0.52
215000 0.45
214500 0.56
2()9150 0.75-
Nil
Nit
NI?
1.9S
1,79
4.90
1.43
1.57
NI?
1.31
1..24
1.24
1.42
1.45
1.71
1:,5
1.75
1.76
1.64
1.99
2.16
1.94
2.00
1.03
1.95
1.92
1.72
1.94
NH
NH
NR
0.55
0.59
1.35
1.16
0.45
Nil
0.61
0.53
0.33
0.29
0.66
1.04
0.-73
0.32
0.27
0.99
0.62
0.70
0.51
0.66- 0.56
0.90- 0:30
0.73 '0.44
0.53 0.70
0.54 0.40
0.66 1.12
1.25 0.50
1.26 0.30
1.55 0.41
0.57 0.59
0.53 0.25
0.77 1.23
0.66 0.37,
1.60 0.35
1.12 0.62
1.04 0.65
1.45' 0.45
2.02 1.22 0.37
1.75 1.26 0.40 ?
1.71 1.21 0.50
1.94. 1.39 . 0.55
1:59 0.99 0.90
1.55 0.92 0.52
1.34
1.54
1.35
2.06
1.95.
2.06
1.52
1.57
1.52
_1.95
1.71
1.51
1.57
1.52.
-1.76
1.55
2.00
1.75
1.64
1.99
2.16
1.94
2.12
1.39
1.01- 0.19
1.55 0.19
0.52 0.09
1.02 0.09
1206
1 '210
1.236
1,.234
1.22 0.08 _1.'249
? 1.74 0.09 1.256
1.25 0.05 1.'240
0.55 0.07 1:251
1.20 0.09 1:256
1.26_ 0.07 _1:247
1.20 0.09 1..-250
1.25 0.05 1,'251
1.57 0.05 1;254
1.35 6.09 1.'255
0.09 1.250
1.45 -0.09 1.256
0.55 0.19 1.256
1.25 0.11 1. 224
1.54 0.06 1.157
1.51 2.11 1 a;,-2.'?
1.27 0.19 1 '236
1.66 0.11 1.-245
0.69 0.11 1.246
1.02 0.17. 1:214
2.06 1.65 0.07 1.245
.2.05 1.46 0.11 1.-243
2.00 1.32 0.07 1 '247
1.95 1.50 0.11 1.255
2.05 1.71 0.11 1. 257
1.55 _1.45 0.11._ 1.'251_
1.79 1.29 0.11 1.-254
2.04 1.49 0.21 1.'239
1.94 1.04 0.09 .1.255 _?
1.75 1.23 0.11 1 "237
1.63 1.20 0.27 1.99 1.72 0.11 1.'255
2.00 1.07 0.565 2.16 1.31 0.18 1.256
1.5, 0.91 0.64 2.25 1.41 0.21 1:256
2.07 0.56 1.11 2.16 1.07 0.21 1.256
2.17 0.47 1.25 2.17 0:92. 0.11 1251
1.47 1.10 0.37 2.23 1.66 0.11 1255
2:03 1.70 .0.65 2.07 1.19 0.15 1,246
1.79 0.61 0.69 2.10 1.21 0.09 1.'251
1.69 1.40 -0.24 1.94 1.70 0.11 1,.254
1.73 0.93 0.60 2.06 1.26 0.21 1.241
-1.67 1.17 0.36 1..69_ 1.51 0.11_1.249
1.67 0.76 0.91 .1.67 0.76 0:11 1:254
1.48 1.03 0.45 1.52 1.17. 0.07 1.244
1.77 0.06 0.90 1177 0.67 0.07 1254
1.61 0.59 0.90 1.76 0.66 0.07 17254
1.55 1.10 0.75 1.94 1.19 0..11._ 1.245
1.57 0.75 1.09 .2.11 1.02 0.09 1:254
1.02 0.90 0..40 1.69 1.29 0.11 1.245
18 1.13 0.50 1.94 1.44 0.11. 1:253
-1.61 0.54 0.29 1.65 1.56 0.11 1253
1.46 0.43
1.65 0.70
1.05 0.23
1.64 1.19
1.67 1.29
1.55 0.53
1,05 1.62 0.57 0.07 1241;
0.96 1.52 0.64 0.07 1.-251
0.46 1.44 0.95 0.07 1 '255
0.22 1.67 1.45 0.11 1:247
0.22 1.95 1._.76 0.09 1.:253
0.75 1.50 1.05 0.07 1.'255
TOP SECRET RUFF
NO FOREIGN DISSIEM
TOP SECRET RUFF
NO FOREIGN DIS5EM
NPIC/TP-17/64
Terrain
Limiting
1'a,,
Frame
'.:
Oe r-
l ap
Cloud
Unk .
Time
S ' rr
Time
SRI"r
Eli,.
Pitch
(All
Minus)
'
Roll
it.o%
(All
Nlinu,)*
(yd,)
Min
Max
A
!din
Max
_'1
Fog
L.xp
D10:1
D10,1
D103
D111
141 Cei 2111 0942 1227 60 49 15 35 -00 06
154 10 1111 0943 120, 61 34 15 26 -00 04
173 09 1111 0944 1232 63 4 15 15 00 11
23 10 3111 2135 0940 07 11 15 04 -00 02
Note NR denote, no reading made
NA denote:, not, a, ailatile
Terrain
NA ' 214500 0.72 1.41 0.63 0:2, 1.93 1.65 0.07 1 "047
NA 216(010 70.,7 1.42 0.55 0;35_ 1.99 _1.64 0.07 1 '247
NA 223000 1.05 1.95 0.87 0.62 0.10 .1.4,, 0.17 1247
NA 7 23050(1 0.65 0.91 0.26 0.65 1.05 0.60 0.19 1 '235
Limiting
D !Aux Ranee
D Min Runge
.Aserage D Max
.AS erage D Min .
D Max iiiInge
D Min Range
A?erage D. Max
A?erage D Min
0.06-0.01
0.12
0.21-1.27 .
0.63
? TOP SECRET RUFF
NO FOREIGN DISSEM '
A,uRSt9Yd, F r Release 2002/07/01 : QI
TOP SECRET RUFF
NO FOR EIGN CISSEM
NPIC/TP-17/64
APPENDIX C. DENSITY READINGS
1. Stellar Index Camera
Density readings were taken on each pass, EP .1000, with an ET attachment and a-0.5 mm
using a Macbeth QuantaLog Densitometer, Model aperture. The values are correlated below.
Frame
Gro,,,. Fog
D49 01 1.56 2.99 :0.34
D49 02 0.91 2.55 0.34
.D49 03 0.9:1 :1.12 0.34
050 04 0.50 2.5,1 0.31
D50 17 0.92 2.57 0.39 '
D52 15 1.04 :1.45 0.25
052 :14 0.09 :1.17 0.25
D5:3 35 0.66 2.T ((.25-
D53 55 1.42 3.39 0,32
D54 56 0.46 2.00 0.25
D54 75 - 0.59 :1.20 0.25
D55 70 0.37 2.33 0..25
D55 113 1.14 3.30 0.25
D56 114 0.90 3.15 0.21
D56 123* 1.07 _ :1.27 0.25
206E 124 Nil - Nil 0.25
.A57 125 Nil Nil 0.31
D61 120 1.24 :1.29 0.27
061 131 1.29 3.30, 0.24
D02 132 1.02 :1.21 0.26
D02 1:17. 0.09 3.10 0.26
D64 135 0.39 2.95 0.27
D64 145 0.50 2.97 0.30
DOS 149 0.56 3.21 0.27
DOG 15S - 0. 5:1 :1.23 0.25
DOG 159 0.:25 1.44 .0.27
DOG 071 1.00. :1.29 0:"5
DOT 172 0.32 2.50 0.27
DOT 156 ' 0.95 3.10 0.25
D65 157 0.29 2.91 0.24
Frar.-Ie
Gross Fog
D65 212 1.04 :3.37 0.27
D69 213 0.05 :3.04 0.27
DOD 229 0.95 :1.27 0.25
D70 230 0.75 _3.29 0.22
D70 244- 1.06 3.35 0.24
071 245 0.3 3.23 - 0.23
D71 . 263 1.05 3.34 0.25
, D72 264 0.9.5 3.34 0.24
D72 .77 0.9S 3.20 0.2S
A72E 27,.7. Nil NI? 0.27
D75 277 1.24 3.45 .0.29
DTs 21 NI? Nil 0.24
D53 25 1.13 3.40 0.26
D53 290 1.51 3.61 0.24
D55 297 Nil Nil 0.24
055 312 NR Nil - 0.25
D513 313 1.04- 2.56 0.05
D50 :129 1.55 3.4S 0.25
D57 :130 1.12 3.25 0.26
D57 34S 1.17 3.43 0.35
D94 349 Nil Nil 0.25
094 355 Nit NI; _ 0.25
D101 356 Nil Nil . 0.25
D101 363 Nil Nil . 0.25
0102 361 NR NI; 0.25
D102 350 Nil Nil 0.25
-\103E 31 NI: Nil .. 0.25
0103 $52 Nil NR 0.25
D103 409 Nil NI: 0.27
Note NI: denotes na reading made
D Max tlange 1.44-3.61 .A?erage D Max
D Min Range 0.2s-1.S1 ANerro,e D Nun - 0.91
Fog flange 0.22-0.39
A% erage Gro,,,, Fog 0.27
2. Terrain Index Camera
Density readings were taken on each pass,- EP 1000, with an ET attachment and a 0.5 mrn---
using a Macbeth QuantaLog Densitometer, Model ---aperture. The values are correlated below.
Terrain
Frame
D Min
- ? Limiting
D Min
Gros Fog
049 01 Nil Nil - 0.34 1.73 - ?(.1)(
3.
0).(5).
049 02 Nil Nil 0.20- ?
0.13 1.77-
049 0
(N11 067
1 Nil
0.16 1.74 0.11
050 ).6 .
04 0.91 0.10
17 0.1; 1.12 1.12 0.07
D50
D52 15
(( )I 0.30.. 116: -; 1.01 0.10
0.30 1.01
0.40
0.17
D52 :14 1.47 1.47 0.07
35 0.17 1.05 0.09
D53 1.05
-..TOP SECRET RUFF
NO FOREIGN DISSEM
TOP SECRET RUFF
NO FOREIGN DISSEM
NPIC/TP-17 /64
Terrain
Limiting
Frame
D Min
053 55 Nil
D54 64 0.31
D54 75 ' 0.47
D55 82 0.25
D55 113 0.31
D56 114 0.23
D56 123 0.26
156E 124 NR
A 56 125 Nil
D61 126 _ Nil .
D61 131 Nil
D62 132 0.25
D62 137 0.14
D64 142 0.15
064 145 Nil
D65 149 0.34
D65 156 0.53,
D6G 163 0.33
D66 169 0.40
D67 177 0.23
_i
D67 1Sa 0.23
DOS 193 0.25
D6S 212 0.60
D69 213 0.20
DO9 229 0.29
D70 220 0.15
D70 244 0.30
D71 245 0.33
D71 263 0.34
D72 264 0.23
D72 .--.77 0.31
172E 27s NI?
D7S 279 0.44
075 254 NR
DS3 253 0.17
D53 296- 0.27
DS5 297 0.22
DS5 312
056 319 0.27
DSC, 326 0.49
D57 330 0.24
D87 345 0.27
D94 349 . ((.1.7
D94 335 .0.27
0101 336 0.25
0101. 363 0.35
D102 372 0.31
0102 3-0) 0.23
.1103E, 351 Nil
0103 409 0.35
1104E 410 - Nil
D111 411 Nil
D111 425 0.39
Note NR denotes no iTading ni,ade
Terrain ?
D Max Range 0.63-1.35
13 Min Range 0.14-0.61
Averai,e D Max 1.11
erage D Min 0.30
Nil Nil 1.35 0.07
0.58 0.31 0.55 . 0.07
1.35 0.47 1.35 0.07
6.74 0.2-5 0.57 0.07
0:95 0.31 1.35 _ 0.07 -
1.10 0.=25 1.13 0.07
1.00 0.26 1.10 0.07
Nil Nil NR 0.07
Nil. Nil NR 0.07
Nil 0.66 1.29, _0.05
NI/ 0.43 1.54 0.05
.-0.9S 0.25 0.95 0.10
0.91 0.14 0.91 0.0
0.70 arei4S 0.85 0.12-
Nil 0.15 1.47 0.11
0.67 0.20 0.70 0.11
1.05 NI? Nil 0.11
1.15 0.22 1.15 0.07'
1.35 0.15 1.36 0.07 .-
1.21 0.23 1.21 0.07.
1.09 0.17 1.18 0.05
1.29 0.25 1.29 0.07
1.22 0,52 1.24 0.07
1.02 0.20 1.06 0.07
1.25 0.29 1.45 0.07
1.31 0.15 1.31 0.07
1.50 0.30 1.50 0.07
0.87 0.33 1.14 0.07
1.09 0.13 1.46 -0.07
1.12 0.14 1.12 0.07
_
1.06 0.31 1.06 0.07
Ni? Nil NR 0.07
1.49 0.44 1.49 0.07
NI? Nil- NI? 0.07
1.170 17 1 17 0.07
. _ - ._ . .
1.10 0.15 1.37 0.07
1.17 0.22 1.17 0.07
1.31 0.26 1.31 0.07
-1.17- 0.27 1.17 0.07
-1.24 _0.49_
0.90 0.24 0.90 0.07
1.55 0.27 1.35 0.07
1.05 0.17 1.05 _0.07
1.05 0.17 1.05 0.07
1.22 0.25 1.22 0.07
1.30 0.35 1.30 0.07
0.65 .0.31.- 1.07 0.07
1.64 0.23 1.64 0.07
Nil Nfl NH 0.07 -
1.17 _. 0.22_ 1.17 0.07 _
Nil Nil NR 0.07
Nil 0.07 0.30 0.07
0..5, 0.39 i 0.82 Q.07
Groi-is Fog Range 0.05-0.11
.1%erage Gross Fog 0.05
Limiting
D Max Range - 0.30-1.77
D Min Range 0.07-0.66
Average, D_Max 1.22
? erage D Min 0.26
A provpci For Relew 2002/071Q A-R P
TOP SECRET RUFF
NO FOREIGN DESSEM
Emuis,on 4404
PA JORAMIC MASTER CAMERA -
it
- EXPOSURE .
Sesitcy:ieteF 19
Exc'es..re T,7e 1 25 sec. .
? PROCESSING Le z 511=1 32
GAMMA . 0.5 G SPEED FOG
214 113 .19
_
'
1.1
. ;
.
'
CONTROL CURVE FOR HEAD AND
TAIL OF MISSION RECORD
..
_a
TOP SECRET RUFF
NO FOREIGN DISSEM
TOP - SECRET RUFF
NO FOREIGN DISSEM
NPIC/TP? 17/64
Emulsion .4.04
PANORAMIC SLAVE CAMERA -
MISSION 1004-
0
EXPOSLAt
Sensitome1er 1B
Exposcre Time 1 25 sec.
PROCESSING Log E11=-1.33
GAMMA 0.6 G SPEED FOG
2.20 1.14 - . . .15
-
,
CD
e
&
,
.
-
11
i
'
-.
CONTROL CURVE FOR HEAD
. AND TAIL OF M SSION RECORD
'
LOG EXPOSURE
.0
NPIC J-000.4 le 'CA)
TOP SECRET RUFF
NO FOREIGN CISSEM
NPIC/TP-17/64 ?
PANORAMIC CAMERA
L?... . ..
?.
-
..,....3.....
-
?
EXPOSURE
Se.cs,lcc?eter IS
Excose Ti:e. 1 25 sec:
PROCESSING 1.-?'6 ' E11 =1
GAMMA 9.5 G SPEED ' FOG
2.29 1.03 .21
?
?
33
,
?
?
.
._
.
.
.
..
...
_
11
-
////e....v......?..,..?..?............----------
?
/
?
SENSITOMETRIO'CURVE FROM
? !ISSION MATERIAL '
t
-
LOG EXPO 'J
.0
NPIS C:GT IC
TOP SECRET RUFF
NO FOREIGN DISSE/.4,
TOP SECRET RUFF
NO FOREIGN DISSEM
NPIC/TP-17/64
INDEX CAMERA
_
_
EXPOSURE
Sens,toc?eter 10 I
Exccsue.Tnne L' ED sec.
PROCESSU,IG Lc 3 Ell= .70
GAMMA 050 SPEED FOG
1.04 2.40 . .07
_
.
?
?
_
,
.
_
,
cat .
_
..
-
.
.
,.
_
11
.
",////
,
1
.
'
,
'
._
'
CONTROL CURVE FOR HEAD
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? TOP SECRET RUFF
NO FOR E1GN Di SSEM
NPIC/TP-17 /64
STELLAR CAMERA
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TOP SECRET RUFF
NO FOREIGN DISSEM -
TOP SECRET RUFF
NO FOREIGN DISSEM-
NPIc/TP-17/.64
APPENDIX D. EDGE SPREAD FUNCTION
In an attempt to establish an objective meas-
urement of image quality in photography, the
technique of obtaining the spread function from
microdensitometric edge traces is being inves-
tigated. The spread function curve represents
the whole photographic system, and is a sum-
mation of the separate elements: lens, film, and
uncompensated image "motion due_ to vibration,
velocity, roll, pitch, yaw, and aerial turbulence.
To assign a single number to the spread
function, the width is measured at SO percent
amplitude. This number, usually expressed in
microns, .may be converted by use of the scale
factors to ground distance in feet.
Edges meeting the criteria described below
have been found in domestic passes of missions
in the same frame as resOlution targets and have
been scanned. The ground distance in feet, thus
determined, has been close to that determined
from the resolution target. Although the tech-
niques used are not refined and are considered
to be still in the development stage, the potential
of this type of objective analysis should be re-
alized. The two examples of edge scans and
their respective spread functions are included as
a preview of this type quality analysis.
Any optical image can be thought of as being
composed of an infinite number of image points
(or lines) of light, each being conjugate with
points (or lines) in the object. While the. object
points can be infinitesimal light sources, the
image points are alWays mounds or distributions
of light having finite size. This blurring of light
points in a photographic system comes from
diffraction and aberration in the lens, light
sprading and diffusion in the emulsion, and
image motion caused by camera movement and
atmospheric shimmering. The fundamental
building block of the image then is the distri-
bution of light in any of the image points. This
distribution is called the spread function of the
photographic system.
Lamberts and others have explained the
mathematical and experimental correspondence
of a sharp edge and its spread function. An
analogy exists in the techniques of studying
electrical system response. The analysis re-
quires that the source or object fulfill the condi-
tions of a unit step function, i.e. exist for an ap-
preciable time or distance at a fixed signal level
and instantaneously or abruptly change to a new
level which is maintained for an appreciable time
or distance. The spread function is obtained by
differentiating the signal output curve point by
point (i.e. measuring the rate of change or sig-
nal with time or distance, and plotting signal
amplitude versus time or distance).
As a-starting point the mission is examined
to locate examples of best photography with
edges long enough and straight enough for use in
the rnicrodensitometer, and having uniform den-
sity on each side of the edge to fulfill the condi-
tions of a unit step function. This requirement
is usually achieved by rooftops of buildings in
large-scale photography, and aircraft runways in
small-scale photographs.
The microdensitometer used is a Joyce-
Lobel Double Beam Model III C. It is used with
an effective slit of one micron by 125 microns_
The recording table and sample table are direct-
ly linked with a ratio arm of 1000:1. The speed
of the scan is variable and is determined by the
amount of pen deflection (as the pen is deflected
the speed decreases giving the pen time to reach
its maximum response). The chart thus pro-
duced represents a plot of chart displacement
versus distance. This plot is manually smoothed
by the analyst and is a judgment of what the edge
would be if grain and other anomalies were
absent.
?? TOP. SECRET RUFF
NO FOREIGN,DISSE.P.
LWJ
TOP SECRET RUFF
NO FOREIGN DESSEM
NPIC/TP-17/64
The data reduction is done manually at pre-
sent, but the feasibility of using the UNIVAC 490
computer is being investigated. The micro-
densitometer calibration curve (chart displace-
ment to density) is used to determine the den-
sities at equal distance increments along the
trace. The I) Log E curve for the material-(den-
shy to log exposure) is used to determine the
Log E and therefore the exposure requtred to
produce the determined densities. The alues
of E are plotted against the distance across the
edge to produce the original scene reflectance
distribution as recorded in the negative. The
final step is a determination and plotting of the
slope of this curve (dE/dX) versus distance, point
by point. This last plot is the spread function
for the whole photographic system. .
The width of the spread function curve is
measured at 50 percent of maximum amplitude
and is indicated on the enclosed traces.
TOP SECRET RUFF
NO FOREIGN DISSEM
Approved For Releese 2002/07/01 : CIA-RDP78T05439A000500050005-0
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Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
25X1
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
TOP SECRET RUFF
NO FOREIGN CISSEM
NPIC/TP-17/64
? APPENDIX E. MISSION COVERAGE STATISTICS
1. Plottable Coverage: The following is a
summary of plortable coverage for this mission
given in linear nautical miles (ln/nm) and in
square nautical miles (sq/nm). The figures are
the sum of both master and slave photography,
and exclude coverage which is entirely over
water or completely cloud covered.11
25X1A
In Table 1, a mean cloud percentage value
has been calculated for each category for use in
determining a combined cloud-cover percentage
for all operational passes of the mission.
The occurrences of each 'cloud category
within an operational pass is expressed as a
percentage and. appears in Table 2. Each per-
centage is a .ratio of the number of occurrences
of a given cloud-cover category to the total num-
ber of cloud observations in a photographic pass.
For example: if the.number of category 1 Oc-
currences in a given pass is 200out of a total of
1000 (250 frames x 4 quarters), all categories
combined, then 20 percent of the pass would be
as in category 1.
A cloud-cover percentage per pass is in-
cluded in the last column of Table 2 under "cloud-
cover percentage per pass." This value is de-
termined by the summation of the products
category percentage in each pass and the mean
cloud percentage for that category as established
in Table 1. For example: it is determined that
the following percentages exist in a given pass:
20 percent
15 percent
30 percent
25-percent
10 percent
Category 1
Category 2
.Category 3
? Category 4
'Category 5
2. Cloud Cover: This statistical analysis of
cloud cover on Mission 1004-2 is based on cloud
coVer per quarter segment of each frame of -
photography. The data are obtained by analysts
trained in estimating cloud cover by designated
categories.
Five cloud categories have been formulated
for use on this photography. These categories
allow for-the wide latitude of cloud-cover condi-
tions commonly found on a frame- of this
photography. covered.
Then, by using the mean cloud percentage
established in Table 1, the following computa-
tions are made:
0.20x 5.0 = 1.00 percent
0.15 x 17.5 = 2.63 percent
0.30 x 35.0 = 11.40 percent
- 0,25 x 75.0. = 15.75 percent
0.10 x 100.0 = 10.00 percent
TOTAL 43.76 percent.
Hence, 43.8 percent of this pass is cloud
TOP SECRET RUFF
NO FOREIGN DISSEM
For Release 2002/07/01 : CIA-R
, ,
TOP SECRET RUFF
NO FOREIGN DISSEM
NPIC/TP- 17/64
TaSle I. Cloud-Corer-Ca tegories:
Category Percent of.Mean Cloud
Descrption
- Number Cloud Cover Percentage
1 Less than 10 Clear 5
10 - 25 Small Scattered 17.5
Clouds
26 - 50 Large Scattered 3S
Clouds ?
51 - 99 Broken or Con- .75
_
fleeted Clouds
5 100 Complete .Over- 100
cast
PCTCC7i1C:;'C of Cloud Corer Categories by Passes
Pass
Number
Cloud-Cover
Percentage
Per Pass
50D 60.6 15.5 12.5 5.1 0.0 17.2
52D 55.9 5.6 3.9 . 1.4 0.0 6.4
53D 31.3 5.7 5.4 7.5 50.1 60..4
54D 62.2 7.3 9.1 11.5 9.6 26.3
?55D 25.5' 20.5 14.9 24.6 10.9 40.1
56D 40,1 10.9 13.7 21.6 13.7 39.0
64D 21.7 35.6 22.5 13.9 3.0 29.9
65D 60.3 3.0 4.7 23.3 5.7 . 31.5
66D 44.9 13,7-' 20.5 20.9 . 0.0 25.1
67D 69.5 4.6 5.7 '19.9 0.0 21.3
GSD 58.3 15.9 9.0 10.9 2.9 .20.7
69D 72.3 19.7 5.9 ' 2.1 0.0 10.9
70D 62.7 10.4 4.0 20.4 2.5 24.3
71D 10.7- 7.5 11.4 22.2 45.2 71.0
.72D 56.3 20.3 15.6 - 6.7 1.1 15.4
63D 79.0 10.2 6.2 4.6 0.0- 11.5
55D 65.3 17.3 9.1 6.1 0.2 16.0
56D 47.2 6.4 3.4 17.6 25.4 43.4
67D 30.4 9.9 11.4 21.5 26.5 50.5
101D 47.9 40.6 -4.5 6.6 0.4 16.5
102D 40.5 9.6 6,2 24.2 19.0 43.3
103D 29.5 14.3 10.9 16.5 15.5 39.5
111D 35.6 37.1 9.3 5.0 0.0 16.2
112D 12.0 8.8 5.6 71,3 2.3 60.0
45-.2* 14.3* 9.6* 15.6* 12.3* -32.5"
*Average Percentage by Category for Mission.
**Overall Mission Cloud Cover Percentage.
a
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Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
25X1D
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
TOP SECRET
NO FCREIGI:i GiSSEM ?
TOP SECRET
NO fORE,GH Or..S[M.
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
25X1
Approved For Release 2002/07/01 : CIA-RDP78T05439A000500050005-0
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14 57
15 JO
1516
15
15 3'.:$
15 42
15 51
16 oU
16 .:j3
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16 25
16 "."3
16 42
16 55
16 53
17 6
17 14
17 22
17
17 36
17 45
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16 23
16 '31
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18 93
19 ?
19 17
19. 14
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19 41.)
1(.) 53
23
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20 16
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TALENT?KEYHOLE
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Control Only _
RH39A000500050005-0
Approved For Release 2041,20E
PASS
DAY MO YR
I ' I VI , 01-1/4.1\i- i ,
? SPECIAL HANDLING REQUIRED ,
.2,31
2...1 :4 6..2.
FRAME
Z TIME
hr mi sec
n
TIME
? piff
mil sec
CAMERA
dog Latitude
min
NADIR
deg Longitude
mi n
FORMAT
Latitude 1
deg mi n
CENTER ?
Longitude
deg . min
ALTITUDE
(ft)
VELOCITY
(ft per soc)
AZIMUTH
deg min
SUN ANGLE
deg min
_
PITCH
dog min
ROLL *
deg . mi n
'7)
6
7
1Ci
11
12
13
14
15
16
17
16
19
4.-
21
'2
24
25
26
27
20
29
31
32
33
34
.39
36
.33
39
41
42
'13
45
46
47
.':11
9267
:3
.7:2
57'2;:
7.12
1Y,,-392
3
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25,126
3'-,941
15 331
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697'.;
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24a26
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',113
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33 23
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14 77
29.471
4 35.Y)1
;/3 426
474:221
51.761
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3 '59 (.":4a566
13 25 .r.,Y.346
15 2: 265
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11
54
59
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53
57
57
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57
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47.28k
22.5f5N
390')IIN
57.11N
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25.91N
41076N
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TOP SECRET
16 10
16 27
16
16 16 114
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17 16
17 26
17 34
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11 17
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21 36
21 42
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PASS
DAY MO YR
33A
4
TIME
Diff
mil sec
CAMERA
Latitude
dog min
NADIR
Longitude
deg min
FRAME
Z TIME
min 50C
1. `,3
5/;
55
S6'
57
59
.6
61 ;;;) A
62
63 :6
04
()7
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69
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60727
4.35
11:07
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427.'...; 65
4.25 UO2,1N
25,CAN
'122 25
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17:)t)::;11fl
1..91N
? (..6 1.3077N
(,6 25047N
4175 (.6 37,11N
(7 22 31:I'
67 13 52
67
54,9-rn
1,1
26043N.
3601.141:
Y!r)074N
560,17N
629
1C;075N
TOP SECRET
SPECIAL HANDLING REQUIRED
FORMAT CENTER
Latitude Longitude
deg min deg min ?
ALTITUDE
VELOCITY
AZIMUTH
SUN ANGLE
PITCH
(ft)
(ft par sec)
deg min
deg min
deg min
1;; 21
14 .'-7N
64l 0
...1.41 41 .22
11
22 19
17N 25
29N
([phone] / L. 2. (.467 .143..>? 7 22 26
22 42
.22677 1Y 22, 22 42
(,)75 1 54
19 21 59
41N [2,
(..() 11)
ci7 .,41 47 2 16
z...7 21,H,r,7 46 27
32
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!..11
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23
21
4:3,
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'56
23
43
?.)732
352.
29
23
53
,51
J2
23
.59
...36
24
;ii?
12
24
ROLL
deg min
Approved For. Release 2002/07/n1 ? rIA-RDP78T05439A000500050005-0
TOP SECRET
PASS
FRAME
DAY MO YR
"?':
Z TIME
hr min sec'
TIME
Mff
mils
CAMERA NADIR
Latitude Longitude
dog min deg min
65? 51
65 1:mal)N.
i:3433N
52,,P(4!
(";:!.
.2).,1411
sss 64
1-57,:)5M
.,r1
(;20
::11/75 61.; C,20YA1
547 (22 D1.1,56N
"./s".7: 1:.;o)1,11
:;4.T., 62 C7,3M
61 !--4',032N
;?)4o26N
C,1
1175
"...r.',65 (I
TOP SECRET
SPECIAL HANDLING REQUIRED
FORMAT
Latitude
dog min
CENTER
Longitude
deg min
ALTITUDE
(ft)
VELOCITY
(ft per sec)
3;
17:1 !AL 6..;(675
27L
1--/V 155. .5-565 262
,,/1
;111.1.
l;
L71
....di:
'
:71
;!IC217
12,2. 7711,
17:.! ".;LL
,
5 173 L. 3ui
17; ..)OL ,122"4:Cii
5. 17M 17.', ,7L
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)5N1.75 :iss 5s5
62 6151 175
rff.: 176 514557 ;Y5.:1
UN 17::
-1,U,
17(, 257551 5251
AZIMUTH
deg min
SUN ANGLE
deg' min
11
12
12
1?)
14
14
lb
15
16
14 ?
'17.
17
17
17.
17
17
15
16
iC
1C.
17
17
17.
PITCH
dog min
ROLL
.cleg min
Approved For Release 2002/07/01 :
Handle Via
IA-RDP78T05439A000500050005-0
TOP SECRET
A 6 A.4.1OO$14.161.01,