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Approved for Release: 2018/09/11 C051 03025 

GAMBIT 

SYSTEM 

PERFORMANCE EVALUATION TEAM 

(FliGHT :MISSION CHARACTERISTICS) 

:MISSION 4022/65 

This report consists of _. 142 pages. 

GROllP 1 

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Cy of 5 copies 

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GAM BI T 

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BCS 39739-65 

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FOREWORD 

TIllS REPORT PREPARED FOR AND BY DIRECTION OF 

THE DIRECTOR OF SPECIAL PROJECTS 

OFFICE OF 

THE SECRETARY OF THE AIR FORCE 

Preparing Unit: 

~-GAMBIT 

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Performance Evaluation Team 

Los Angeles AF Station 

Los Angeles, California 90045 

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, 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

PUBLICATION REVIEW 

This report has been reviewed and is approved. 

VICTOR M. GENEZ 

Colonel, USAF 

Team Manager 

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REPORT NO. 4022/65 

TITLE PAGE 

FOREWORD 

PUBIJCATION REVIEW 

TABLE OF CONTENTS 

LIST OF ILLUSTRATIONS 

LIST OF PHOTOGRAPHS 

TABLE OF CONTENTS 

SAFSP PERFORMANCE EVALUATION TEAM ........................... . 

Page 

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SECTION I - RESUME OF MISSION 4022. • . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 

SECTION IT - FLIGHT PROGRAM ................................. . 

SECTION III - PHOTOGRAPHIC CHARACTERISTICS EVALUATION SUMMARY .... . 

SECTION IV - CAMERA SYSTEM OPERATIONS ........................ . 

SECTION V - VEHICLE POSITIONING· .............................. . 

APPENDIX A - TECHNICAL DATA SHEETS ............................ . 

APPENDIX B - PHOTOGRAPHS ..................................... . 

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Number 

1 thru 8 

9 thru 14 

15 thru 17 

18 thru 21 

22 thru 27 

28 thru 29 

30 

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LIST OF ILLUSTRATIONS 

MISSION PLOTS ............•..•.•.....•.....••.• 

STELLAR INDEX CAMERA INDEPENDENT OPERATIONS ..... 

FILM VELOCITY PLOTS ............•.•............ 

PLOTS OF TEST CASE RESULTS .................... . 

ST ATISTICAL PLOTS OF MISS DISTANCES .........•..... 

EXAMPLES OF ATTITUDE VARIATION ON LONG FRAMES ... . 

VEHICLE ATTITUDE CHART ....................... . 

TOP SECHKT..- GAMBIT 

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Page 

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13 thru 18 

25 thru 27 

75 thru 78 

79 thru 84 

85 thru 86 

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REPORT NO. 4022/65 

Number 

1. 

2. 

3. 

4. 

5. 

6. 

7. 

8. 

9. 

10. 

II. 

12. 

13. 

14. 

LIST OF PHOTOGRAPHS 

CORN TARGET AT WELLS, NEVADA (SFO 109-1) .................... . 

CORN TARGET AT GREEN RIVER, UTAH (SFO 109-2) ................. . 

BLUEBIRD PHOTO OF CORN TARGET AT ELOY, ARIZONA ............. . 

CORN TARGET AT ELOY, ARIZONA (SFO 109-3) ..................... . 

CORN TARGET AT LOWRY AFB, COLORADO (SFO 109-4) .............. . 

BLACKBIRD PHOTO OF CORN TARGET AT BOONEVILLE, MISSOURI ...... . 

CORN TARGET AT BOONEVILLE, MISSOURI ....................... . 

CORN TARGET AT OLNEY, ILLINOIS ..........•.................. 

CORN TARGET AT MATHISON, MISSISSIPPI ..•...•................. 

CORN TARGET AT NORCROSS, GEORGIA ......................... . 

CORN TARGET AT HILL CITY, KANSAS (GLASS BLOCKS TEST SLIT) ...... . 

CORN TARGET AT HILL CITY, KANSAS (GLASS BLOCKS TEST SLIT) ...... . 

CORN TARGET NEAR BIG SPRINGS, TEXAS (GLASS BLOCKS TEST SLIT) ... . 

RADIO TOWERS AND BRIDGE AT MILWAUKEE, WISCONSIN (MISSION 4017) .. . 

15. RADIO TOWERS AND BRIDGE AT MILWAUKEE, WISCONSIN ............ . 

16. GAS STORAGE TANK AT CHICAGO, ILLINOIS (MISSION 4017) ............ . 

17. GAS STORAGE TANK AT CHICAGO, ILLINOIS ...•...•............•.. 

18. FOOTBALL STADIUM WITH GAME IN PROGRESS, CHICAGO, ILLINOIS .... . 

19. MIDWAY AIRPORT, CHICAGO, ILLINOIS ......................... . 

20. HANGAR BUILDINGS AT LOWRY AFB, COLORADO ....•...........•.. 

21. DRIVE-IN THEATRE AT PHENIX CITY, ALABAMA 

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B-2 

B-3 

B-5 

B-6 

B-8 

B-10 

B-12 

B-14 

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REPORT NO. 4022/65 

SAFSP PERFORMANCE EVALUATION TEAM 

SAFSP 

Col Victor M Genez 

Col Kenneth R Duncan 

Lt Col Gonzalo Fernandez 

Maj David B Coleman Jr 

Maj Bernard W Quinn 

Maj Sam R Sci otto Jr 

6594th TEST SQUADRON (AFSPPL) 

Col Harold Z Ohlmeyer, Commander 

Technical Staff 

DET 1, AIR FORCE SATELLJTE CONTROL FACILJTY (AFSCF) 

Lt Col John C Tracey 

Lt Richard K Stearns 

NPIC 

ACIC 

Mr Randall F Gehrke and Associates 

AEROSPACE 

Dr Robert C Hansen 

Dr Lawrence J Vanden Bos 

Mr John Luecht 

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BCS 39739-65 

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REPORT NO. 4022/65 

A. INTRODUCTION 

SECTION I 

RESUME OF MISSION 4022 

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Mission 4022, consisting of the GAMBIT Camera system and the Orbital Control Vehicle (OCV), 

was launched into orbit from Point Arguello Launch Complex, Pad 3, at 1223:38Z on 30 September 1965. 

B. OBJECTIVES 

The operational objectives of this mission were to conduct: 

1. A four-day reconnaissance mission to obtain high resolution photography of specific targets 

selected by the NRO staff. 

2. R&D experiments to obtain exposure and filter data using special test filter configurations in 

Slit position A. 

3. Continuing R&D experiments to evaluate focus sensor mechanism, film set data, exposure I tests, inner shield operations, thermal control, OCV power supply, capability of augmented tracking 

stations to support orbital operations, and BUSS capabilities. 

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4. Fifth day OCV solo operations to demonstrate vehicle attitude control and full system 

capability over a five day period. 

C. MISSION INFORMATION 

1. Powered Flight and Orbital Parameters 

The Standard Atlas/ Agena combination which boosted the satellite into orbit had the following 

powered flight ascent parameters: 

NOMINAL (SEC) 

BOOSTER ENGINE CUT-OFF T -I 132.40 

BOOSTER ENGINE JETTISON T -I 135.40 

SUST AINER ENGINE CUT-OFF T -I 273.92 

VERNIER ENGINE CUT-OFF T -I 293.60 

BOOSTER SEPARATION T -I 296.10 

AGENA IGNITION T -I 331. 17 

AGENA CUT-OFF T -I 566.89 

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ACTUAL (SEC) 

~:; T -I 130.14 

T -I 133.35 

T -I 280.05 

T -I 298.71 

T -I 301. 21 

T -I 337.14 

T -I 575.04 

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The satellite (OCV) achieved a near-nominal orbit with the following elements: 

NOMINAL ACTUAL 

INCLINATION (DEGREES) 95.5 95.56 

PERIOD (MINUTES) 88.85 88.91 

PERIGEE (NM) 85.9 85.05 

APOGEE (NM) 157.11 160.8 

ECCENTRICITY .0095 .0098 

ARGUMENT OF PERIGEE 

(DEGREES) 137.44 141. 67 

2. Recovery 

The capsule was de-orbited on 4 October 1965 on Rev 67 and was. recovered by air catch. The 

OCV solo exercise was terminated four revs early due to power depletion. The OCV was de- boosted on 

5 October on Rev 77 with impact predicted in the South Atlantic at 16° 22'N 32° 25' W. 

D. RESULTS 

The operational objectives of Mission 4022 were satisfactorily accomplished despite the fact that 

high stabilization control gas consumption required budgeting on Day 4 and resulted in the elimination of 

some low priority primary targets as wen as several R&D operations. This mission resulted in a total 

of 198 stereo pairs, 95 framed stereo pairs, 9 lateral pairs and 206 strip frames utilizing 2699 feet of 

film in the primary camera. The GRAVY program indicates that a total of 963 COMOR targets were 

available, of which 543 were photographed in cloud free areas. (See NPIC comments below.) 

E. ANOMALIES 

Only one serious anomaly was noted: 

An apparent high consumption rate of stabilization control gas required the reduction of roll 

maneuvers on Day 4. The unscheduled depletion was apparently caused by a high rate of usage by this 

vehicle for orbit stabilization maintenance as well as the increase in numbers of a new target category 

type. This problem is under study by the contractor for development of specifiC procedures which will 

prevent a recurrence of unscheduled depletion. Completion of the study is scheduled prior to the next 

mission. 

F. OVERALL EVALUATION 

The follOwing subjective evaluation of Mission 4022 is submitted by the National Photographic 

Interpretation Center (NPIC). 

1. The intelligence content of the Mission is one of the highest to date with 543 targets covered in 

cloud-free or partially cloud-free areas. Most of the important targets were covered with stereo I photographs. This target coverage was equivalent with the best previous missions that were of four day 

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duration, but not numerically equivalent to a five day mission. 

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2. The photo interpretation of this mission was the best to date of many of the prime targets that 

must be covered for intelligence purposes. Most of the prime targets were covered with stereo photographs 

and proved to be the best photography of the target areas gained to date. The target portion of the readout 

has been separated into two separate readouts and since the second readout is incomplete at this time 

the number of targets quoted is subject to change. 

3. The acquisition of targets was exceptionally high with no misses due to attitude or coordinates. 

The only limiting factor to a higher acquisition was the 50% cloud cover experienced in the target areas. 

4. The mensuration of imagery on this mission was the best to date and was enhanced by the fact 

that the stellar/index package worked throughout the mission and adequate stars existed on 1304 frames 

of the 1767 exposures programmed. Stellar reduction was possible on all of the frames with adequate 

stars. The mensuration of imagery with known dimensions with accurate camera attitude was within 1/4 

of 1 percent on all dimensions long enough to minimize pointing errors and resolution limitations. 

5. The film speed variations on this mission were higher than on some previous miSSions but 

were generally within the 1% area of the programmed speed. Some excursions beyond the 1% lines do 

occur but do not seem to degrade the imagery when viewed through high magnification. The excursions of 

the film speeds from nominal or programmed values was generally within plus or minus 1/2 of 1 percent 

of the programmed value. The settling times at the start of the frames were approximately. 4 seconds 

with a significant change at about 1. 2 seconds after the start of the frame. The rest of the speeds were 

within the limits stated above. The looper actions were normal to the previous missions with no variations 

outside the plus or minus 5% lines except at the very start of the looper area. The looper area extended 

through about 3.8 to 4 seconds in most cases and did not appear to be as violent as it has been on some 

previous missions. 

6. The imagery on this mission was the best achieved to date and was consistent throughout the 

mission. There was a slight fall off in resolution before the two focus adjustments but the imagery was 

relatively consistent from pass to pass. Comparison of the same images from Missions 4016, 4017, and 

4018 shows that this mission was slightly better than the previous best missions. The best resolution for 

this mission was about 1. 8 feet with the average ground resolution being about 2.0 feet. Mensuration 

techniques for producing ground resolution show some areas where the resolution reaches 1. 8 feet but 

the resolution decreases in a normal fashion when high obliquity angles occur or with the higher altitudes 

in some portions of the mission. CORN Target readings were consistent with the mensuration figures 

above. 

7. The time track operated continually throughout the mission and provided the accurate 

mensuration base necessary in this type system. The yaw slits operated throughout the mission and 

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provided some yaw checks against the stellar reduced yaw. 

8. Stellar /Index Camera 

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a. The Stellar /Index camera operated throughout the mission in both the dependent mode 

(with the main camera) and the independent mode for mapping purposes with no master camera operations, 

b. There were 1771 programmed frames of which 1767 were acquired. Both the stellar and 

index acquired the same number of frames and were correlated by both time and pass number. There 

were 408 frames taken with the vehicle in a positive roll position and the stellar had no chance to acquire 

stellar fields; of the remaining 1359 exposures 1304 had adequate stars for stellar reduction. This is I the best operation of the stellar/index package to date and the stellar field generally contained 10 or more 

stars. High amounts of background light limited the stellar exposures to small areas near the edge of the 

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frame in many cases and these do not contain the best geometry for reduction but can be reduced in a two 

star solution. The flared portion of the format was the smallest to date and the overexposure areas were 

smaller than on previous missions. There are 25 frames with streaked stars due to the vehicle rolling 

during exposure. These have all been correlated to programmed roll conditions and were caused by a 

lack of time between exposure cycles to complete the stellar exposure before the vehicle motion was to I occur. No double exposures were found in this camera. There were four commanded stellar index firings 

which did not occur. 

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c. Time correlations were accomplished by both the M. C. D. and the Telemetry times and 

they both agreed except for the four commanded frames which did not occur. 

d. The final analysis of the stellar fields in the vertical mode and the rolled position of -6.5 

degrees from the vertical have not been completed but it appears that the stellar field recorded is slightly 

better in the -6.5 degree roll pOSition. 

e. The index camera provided excellent coverage of some unmapped areas of the world and 

should prove invaluable to the mapping community. 

9. A final analysis of the mission shows the following facts: 

a. The number of targets covered were comparable to any other four day mission. 

b. The resolution was the best of any mission to date. 

c. The stellar/index operation was the best to date. 

d. The time correlation was the most accurate to date. 

e. The intelligence content was higher than any previous mission due to the higher resolution. 

f. The resolution was consistent and relatively constant throughout the mission. 

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roP tJJ3SPET - GAMBIT -

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1 OCTOBER 65 Z 

2 OCTOBER 65 Z 

3 OCTOBER 65 Z 

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MISSION 

SIC OPS 

13,14,15 

29,30,31 

45,46,47 

61,64 

4022 

1 OCTOBER 

2 OCTOBER 

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MISSION 4022 

SIC OPS 

13,14,16,17, 1 OCTOBER 65 Z 

2 OCTOBER 65 Z 

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__________________ ---1.A~p~p~r~ov~e~d~f~o'_'___r__'_..:R~e~le~a~s~e:~2~0~1~8~/0~9"__/1_'_1'__C~05"'_1_'__'0""'"3'_"0 ..... 2~5 __________________ ._.~ .. 
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SECTION II 

FLIGHT PROGRAM 

Performance of the Command System 

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1. For Mission 4022 all commands, except for those in conjunction with R&D experiments, for 

camera payload operations were generated by the Mission Profile Generation Program (TMPGP) and programmed through the GMINT and GCOMMAND modules. The following table summarizes the command I messages loaded, the rev and tracking station for loading, the operating rev (s) and the results. 

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MESSAGES 

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loa 

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11a 

LOAD REV 

& STATION 

4/POGO 

6/BOSS 

a/COOK 

10/HULA 

14/POGO 

16/POGO 

19/POGO 

22/BOSS 

25/KODI 

30/POGO 

33/POGO 

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COMMAND LOAD SUMMARY 

OPERATING 

REV(S) 

4 

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a 

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PAIRS 

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I REPORT NO. 4022/65 

I LOAD REV OPERATING STEREO FRAMED LATERAL 

MESSAGES & STATION REV(S) PAmS STRIPS STEREO PAffiS PAIRS 

I 121 36/POGO 36 3 1 

37 2 3 2 

122 38/POGO 38 4 11 5 

I 39 4 8 1 

40 5 3 2 

I 123 41/KODI 41 9 8 7 1 

42 12 11 6 

43 11 5 2 1 

44 1 2 

I 125 46/POGO 47 5 3 1 

48 3 3 1 

I 126 49/POGO 49 1 

50 2 

I 127 52/POGO 52 2 1 1 

53 7 1 

I 128 54/BOSS 54 8 12 6 

55 4 8 3 

56 5 9 3 

57 4 6 2 2 

I 129 58/HULA 58 9 2 

I 130 59/HULA 59 1 2 

132 63/POGO 63 4 1 

64 2 3 1 

I 2. Stellar/Index Camera (GSIC) operations independent of the primary camera were programed 

for mapping purposes. A total of 27 command messages were manually programed for independent 

I GSIC operations on 59 revs to obtain 979 photographic frames in the mapping mode. A total of 792 

GSIC photographic frames were obtained during primary camera payload operations. For evaluation, 

I see NPIC comments in Section I. 

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SECTION III 

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PHOTOGRAPIllC CHARACTERISTICS EVALUATION SUMMARY 

(SPPL Report No. 101-1-58) 

I The following observations result from analysis of the original negatives from Reconnaissance Satellite 

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Mission 4022. 

A. Physical Degradations 

1. Imaged 

a. Two fine-lined, continuous minus-density streaks were visible paralleling the major 

axis, approximately 1 1/2" from the titled edge, throughout this Mission. 

b. Dendritic fogging (static discharges) was observed intermittently along the titled edge I of the following Revs: D06, D07, D13-D15, and D52-D56. 

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2. Superficial 

a. A thin, continuous base scratch occurred, approximately 2 3/4" from the non-tttled 

edge on all frames and revs throughout the Mission. 

b. Two emulsion digs, approximately 1/8" in length, were found on Frame 003 of Rev 

D05. 

c. A pre-processing splice (sonic) was noted 4" from the head of Frame 006, Rev D09. 

d. Numerous pinholes were visible on Frame 014, Rev D08 and throughout all frames 

of Rev D07. 

e. A 1/16" wide base scratch was observed extending the entire length at the center of 

Frame 004, Rev D16. 

f. A few minor abrasions, scratches and pinholes were noted throughout this Mission. 

B. Film Format Characteristics 

The titling, time tracks, and fiducial lines appeared clear and distinguishable throughout I Mission 4022. 

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C. Density 

There were 648 density measurements accomplished on Mission 4022. The results are portrayed 

by range, average, and standard deViation «(1) in the following table: 

Dmin 

Dmax 

D 

AD 

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Range Average 

0.22 - 1.30 0.48 

0.34 - 2.66 1. 35 

0.30 - 1. 56 0,92 

0.06 - 2.26 0.88 

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Standard 

Deviation «(1) 

0.17 

0.42 

0.24 

0.42 

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A. Primary Camera 

1. Film Transport 

SECTION IV 

CAMERA SYSTEM OPERATIONS 

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Velocity plots by NPIC showed that this transport system was not as smooth as others. 

Although there are many deviations from the ::-1% film velocity error permitted by specification, the 30" 

value lies well within the specified limits. The looper empty and start of refill did not result in velocity 

variations as violent as experienced previously due to excellent damping. The start up and stopping 

transients were nominal. 

2. Yaw Slits 

Slits were clean and produced usable imagery for image motion analysis. 

3. At liftoff, 2683 feet were available for on orbit use. The load in the supply prior to going 

to the launch pad was 2955 feet. Thefilm was consumed as follows: 

4. 

Pad Checkout 272 feet 

Orbital Health Check 35 feet 

Operational Footage 1223 feet 

R&D/ CORN 376 feet 

Runout 649 feet 

Processing Blanks 400 feet 

Total 2955 feet 

Processing 

Approximate percentages of the use of the three proceSSing levels: 

Full 

Intermediate 

Primary 

72% 

20% 

8% 

Due to misidentification of looper marks for frame lines, some frames received two levels of processing. 

FM-23 will have interframe marks on the film and will eliminate this difficulty. Only one frame could be 

identified as underprocessed. 

5. Exposure 

Optimum exposure occurs about 0.50 density level for Dmin for this mission. Many 

frames have Dmin values below this level but are still within the half photographic stop below D :: O. 50 

deemed as acceptable exposure. About 12% of the frames were below this minimum acceptable level. 

This is due in a large part to the low sun angles encountered this time of year and the terrain sUll covered 

with dark green vegetation. This filter-lens combination has poor green transmission. 

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6. Resolution 

Resolution was the best achieved to date. CORN target readouts indicated levels of about 

1. 8 feet. These readings still must be adjusted for their position in the field of the lens and the higher than 

2:1 contrast of the CORN target as it appears at the aperture of the orbiting lens. This resolution was 

totally unexpected if judgement is based on the tri-bar readings of resolution obtained during acceptance 

testing and MAB validation testing. These levels were about 125 lpm at 2:1 contrast. Besides this 

consideration, the lens was more astigmatic than any other flight model accepted. One theory is based in 

the lack of adequate stiffness in the substrate as compared to later stiffer mirrors and the relieving of 

stress in the zero-G environment. Focus sensor operations indicated BPF as being removed from the 

preflight setting by about. 002". Platen movements on orbit were accomplished moving the platen in two 

separate movements of about. 001" each. No real improvement in resolution as a result of these movements 

is apparent in the preliminary subjective visual analysis nor the CORN target readings. Edge Trace data 

has not yet been compiled at this writing. See NPIC comments on resolution. 

B. Stellar/Index Camera 

S/I No. 18 was flown. No shutter or transport anomalies due to mechanical operation were 

noted. However, four programmed frames about the middle of the mission did not occur. No explanation 

can be offered at this time. A new stellar baffle installed for this mission aided in obtaininga greater 

stellar count than on any other mission. See the NPIC comments on the results of the S/I performance and 

the resulting utility for mensuration. 

C. Experimental Operations 

The following Secondary Flight Objectives were accomplished: 

1. SFO 120: Remote Focus Record - with the door open, no film transport, the focus sensor 

is turned on. Resultant readings were obtained on nineteen revs. These resulted in the platen being moved 

about. 001" on Rev 22 and the same amount on Rev 35. The evaluation of the resulting image acuity has 

not been completed but did not result in a degradation as a result of the platen movements. 

2. SFO 109: Thermal Pulse Degradation of Optics - with the door open for varying periods of 

180 seconds to 800 seconds, strips are photographed at the termination of these door open periods. Edge 

Trace evaluations have not been completed. Subjective judgements indicate little noticeable difference in 

image quality even at the end of the longest period. 

3. SFO 137: Film Set Elimination Experiment - two 1. 9 seconds of film transport operation 

separated by 23 minutes before the processing blank were programmed on four revs. Film velocity plots 

of these frames have not yet been completed. 

4. SFO 138: Slit Change Within Stereo Pair - this was accomplished on Rev 34 between 002 

and 003. Subjective evaluations will be completed by the payload contractor. These evaluations should I indicate to some extent the tradeoffs between reducing smear at the expense of low light detail rendition. 

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5. SFO 139: Move Platen. 002" Between Frames - this was accomplished on Rev 63. Platen 

was moved out on frame 003 and back to BPF on 004. Edge trace data is undergoing processing. Slit 

No. 3 with the glass blocks either side of the center of the slit was used, Subjective evaluation shows little 

change of image quality even though the BPF is increased about. 002" by these glass blocks. 

6, SFO 141: Test Slit Spectral Filtration - the test slit Position A on the slit aperture plate I had four filters across its aperture. This slit was used on six revs. Tone traces were taken from good 

imagery on four revs. Edge traces were taken where well-defined images existed. This data will be 

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reduced at a later date. The configuration of the slit was as shown below: 

Time Track 

Side 

WraUen 

Filter 

50% Trans. 

Slit Width 

2E 

430 m/1 

.0069" 

CORN Targets were obtained on: 

Rev 15, Frame 007 

Rev 16 Frame 003 

Rev 31 Frame 004/005 

Rev 31 Frame 006 

Rev 32 Frame 003 

Rev 32 Frame 006 

Rev 47 Frame 009 

Rev 63 Frame 004 

Rev 64 Frame 00B/009 

Rev 64 Frame 010 

4 

475 mjJ. 

,007B" 

12 

520 mjJ. 

• 00B5" 

Booneville, Missouri 

Wells,Nevada 

Olney, Illinois 

Mathison, Mississippi 

Green River, Utah 

Eloy, Arizona 

Norcross, Georgia 

Title 

Side 

Mechanicsburg, Pennsylvania 

Hill City, Kansas 

Big Springs, Texas 

Polaroid 

All A 

.0204" 

Blackbird aircraft was flown on 1, 3, and 4 October. The coverage obtained on 1 October was 

useful for comparison with Rev 15, frame 007, at Booneville, Missouri. On 3 October there was a camera 

mount and camera malfunction. On 4 October the coverage was two miles west of the CORN targets. 

Blackbird used KA-2, 12" focal length, and T-ll, 6" focal length cameras at 16,500 feet and B, 000 feet 

altitudes. Bluebird aircraft was flown on 2 October. Comparison cover with Rev 32, frame 006, was 

obtained. Bluebird used a 12 inch focal length, KA-53 camera at 1B, 500 feet altitude. 

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ILLUSTRATION 15 

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:-

'" 

<t; '" .. + <t; '" 

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ILLUSTRATION 16 

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REPORT NO. 4022/6r=-5 ______ --,.. ___ ---,m-_---, _______ .... 

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ILLUSTRATION 17 

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PHOTOGRAPH NO.1 

SFO 109-1 

CORN Target at Wens, Nevada 

Door open 301 seconds, focus power on 

Rev D16 

Altitude: 85.7 NM 

Scale: 1:83,200 

40X 

Frame 003 

Obliquity: -12.3° 

Strip 

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REPORT NO. 4022/65 

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PHOTOGRAPH 1 

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PHOTOGRAPH NO.2 

SFO 109-2 

CORN Target at Green River, utah 

Door open 500 seconds, focus power on 

Rev D32 

Altitude: 84.8 NM 

Scale: 1:80,500 

40X 

Frame 003 

Obliquity: + O. 4° 

strip 

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REPORT NO. 4022/65 

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PHOTOGRAPH 2 

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PHOTOGRAPHS NO. 3 & NO. 4 

CORN Target at Eloy, Arizona 

PHOTOGRAPH NO.3 

Obtained by Bluebird aircraft 

using aKA-53, 12" focal length 

camera from 18, 500 feet 

20X 

PHOTOGRAPH NO.4 

SFO 109-3 

Door open- 592 seconds, focus 

power on 

Rev D32 

Altitude: 84.4 NM 

Scale: 1:80,000 

40X 

Frame 006 

Obliquity: -1. 9° 

Strip 

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PHOTOGRAPH 3 

33 

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Afnroved for Release: 2018/09/11 C051 03025 

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PHOTOGRAPH NO.5 

SFO 109-4 

CORN Target at Lowry AFB, Colorado 

Door open 701 seconds, focus power on 

Rev D48 

Altitude: 84.4 NM 

Scale: 1:80,500 

40X 

Frame 011 

Obliquity: + 6. 0° 

Strip 

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PHOTOGRAPHS NO. 6 & NO. 7 

CORN Target at Booneville, Missouri 

PHOTOGRAPH NO. 6 

B.1ackbird photography obtained by KA- 2/ 

12" focal length camera from altitude of 

16,500 feet. 

PHOTOGRAPH NO. 7 

Rev D15 

Altitude: 85.4 NM 

Scale: 1 :81,000 

40X 

Frame 007 

Obliquity: -1. 10 

Strip 

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PHOTOGRAPH 6 

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BCS 39739-65 Approved for Release: 2018/09/11 C05103025 

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PHOTOGRAPH NO.8 

CORN Target at Olney, lllinois 

Rev D31 Frame 005 

Altitude: 84.8 NM Obliquity: + O. 2° 

Scale: 1:83,200 Stereo 

40X 

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PHOTOGRAPH NO. 9 

CORN Target at Mathison, Mississippi 

Rev D31 

Altitude: 84.4 NM 

Scale: 1:80,000 

40X 

Frame 006 

Obliquity: + O. 9° 

Strip 

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PHOTOGRAPH NO. 10 

CORN Target at Norcross, Georgia 

Rev D47 Frame 009 

Altitude: 84. 1 NM Obliquity: -2.6° 

Scale: 1:79,800 Strip 

40X 

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PHOTOGRAPH NO. 11 

CORN Target at Hill City, Kansas 

This CORN target was located in the center of the 

format using the glass blocks test slit. Focal 

plane is at best plane of focus (BPF). 

Rev D64 

Altitude: 84.1 NM 

Scale: 1:83,000 

40X 

Frame 008 

Obliquity: + 5.8° 

Stereo 

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PHOTOGRAPH NO. 12 

CORN Target at Hill City, Kansas 

This CORN target was located in glass block 

adjacent to center block (time track side) using 

glass blocks test slit. Focal plane is at 

BPF + . 0025 in. 

Rev D64 

Altitude: 84.0 NM 

Scale: 1:82,900 

40X 

Frame 009 

Obliquity: + 5.8° 

Stereo 

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PHOTOGRAPH 12 
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BCS 39739~65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

PHOTOGRAPH NO. 13 

CORN Target near Big Springs, Texas 

This CORN Target was located two glass blocks 

from center block (time track side) using glass 

blocks test slit. Focal plane is at BPF + • 002 in. 

Rev D64 

Altitude: 84.0 NM 

Scale: 1:80,000 

40X 

-

Frame 010 

Obliquity: + 5. 8° 

Strip 

T'coiIpr-sSEEeC11R~];i;;;':;]T~- GAMBIT 

- Approved for Release: 2018/09/11 C051 03025 

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BCS 39739-65 

Approved for Release: 2018/09/11 C05103025 ~C1{.I:~.d· - liAMtllT 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

lOP S}!;CBET - GAMBIT -

Approved for Release: 2018/09/11 C05103025 

PHOTOGRAPH 13 

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Aporoved for Release: 2018/09/11 C051 03025 10..1.&...1""' ...... .&...1..1. - '\".A.c&J.Y.LJ.J.LA 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

1. Ephemerides 

SECTION V 

VEHICLE POSITIONING 

a. Generation of Best Fit Ephemeris 

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The Best Fit Ephemeris was generated by reprocessing the tracking data in approximately I one-day spans. Resulting range residuals were generally well under 1000 feet. 

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The following chart shows the fit spans selected for each primary BFE. Included in the 

chart are the weighted R. M. S. residual of the fit (a measure of quality), and the derived drag factor 

(CDA/2m). Nodal crossing time comparisons are also shown for revs common to two fits, to indicate the 

degree of consistency between ephemerides. 

FIT 

SPAN 

1-18 

17-29 

26-34 

32-49 

54-64 

CHARACTERISTICS OF BEST FIT EPHEMERIDES 

PAYLOAD RMS DRAG FACTOR 

REVS* RESIDUAL (FT2/SLUG) 

4-17 1. 22 .1628 

18-27 1. 03 .1769 

28-33 0.83 .1984 

34-49 1. 20 .2003 

56-64 1. 17 .1889 

NODAL CROSSING 

TIME COMPARISON 

. 048 sec @ Rev 18 

.034 sec @ Rev 28 

.030 sec @ Rev 34 

. 013 sec @ Rev 56 

*Revs used for payload analysis runs in TDATA and TEAR routines. BFE was broken into shorter fit I spans due to unusually high magnetic storm activity. 

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2. Map Match 

Forty-nine revs of photography, composed of 813 frames, were available for analysis. To 

improve the reliability of the results and reduce the map error contribution to the overall system error, 

no bench marks were selected on maps with positional error greater than 2000 feet on the World Geodetic 

System. This criteria of selecting photography in areas of less than 8/10 cloud cover provided 1711 bench 

marks on 305 frames of photography. After editing, 1658 bench marks were used for making final analysis. I This photography was located on 39 of the 49 revs taken. 

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3. Position and Attitude Determination 

a. The TEAR Program was used for the Mission 4022 evaluation. The TEAR program 

utilizes data derived from comparing ground bench mark positions common to the map and the photography, 

as well as vehicle (exposure station) positions from either the operational command or best fit ephemeris 

to determine in-track and cross-track miss distances. This is accomplished by using the satellite position 

and tracing the ray corresponding to the photo bench mark (PBM) position on the film through the camera I system to the ground. The difference between the ground coordinates of the traced ray and the PBM map 

I Handle via Byeman 

Controls Only TOP SECRE-1! - GAMBIT 

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Approved for Release: --2018/09/11 C051 03025 ~.c."""'..I."ol.:J.a. - '-X.n.J.V..I..IJ..I..L 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

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coordinates is then resolved into in-track and cross-track miss distances. Thus the miss distances can 

be written 

a = f (A, E, C, M) 

where A, E, C and M respectively refer to attitude, ephemeris, camera and map quantities. Therefore, 

using the programmed attitude and camera orientation, the command or best fit satellite position along 

with the PBM position on the film and the map, the miss distances can be calculated. These miss distances 

(a x and a y) are determined for each PBM in the frame and represent the total system error, the components 

of which are attitude, ephemeris, camera sUb-system and map errors. Using TEAR with the vehicle 

position derived from the command ephemeris, the ephemeris error will contain a contribution due to 

predicting the ephemeris beyond the orbit determination (tracking data) fit span. 

While the miss distances are computed for each PBM, the ultimate goal is to determine the errors 

which caused these miss distances. Knowing the functional relation a = f ( ) the difference equations 

b.a= ~ b.A+ ea b.E + ea b.C +~ b.M = a 

eA eE ec eM 

can be formed where the b. quantities represent the errors (actual value-programmed value) which are to 

be determined and the coefficients of these errors can be explicitly derived. Obviously b.a = a since the 

programmed miss distance is zero. 

In a simplified form to explicitly show the attitude and instrument errors the equations for the down I range and cross range miss distances can be expressed as follows 

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where 

h 

a x 

a y 

a 

xo 

a

yo 

1V 

e 

!J 

cp 

!J + e (1 + ...,;.ta....:n=-:2::--X=---.) + fI) tan X sin !J 

a x = a xo + 1/1 tan cos2 !J T cos2 !J 

1 + b.X 

cos2 X cos!J 

tan X 

a =a +1V 

y yo cos !J 

_ e tan X 

cos2 !J 

sin !J 1 - <1>---

cos2 !J 

Altitude above horizontal plane passing through the bench mark. 

In-track miss distance divided by h. 

Cross-track miss distance divided by h. 

Mapping, timing and ephemeris error contribution to a x divided by h. 

Mapping, timing and ephemeris error contribution to a y divided by h. 

Vehicle yaw. 

Vehicle pitch. 

Vehicle obliquity angle = vehicle roll angle + mirror crab angle. 

Vehicle roll error. 

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Controls Only ~-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

(1 ) 

(2) 

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Approved for Release: 2018/09/11 C051 03025 ~.a. ~..It...JI"""'.L""..L.J"'" 'Io,."A"' ... .I..'IJ..a........,.a. ..... 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

X Calibrated mirror stereo angle. 

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Difference between actual and calibrated mirror stereo angle. 

These equations have been derived for an ordered body orientation of yaw, pitch then roll and small 

angle approximations have been used. In particular, the errors have been regarded as small so that for 

example 

F(D±CP) 

F(X±AX) 

F(D) 

F (X) 

Where F ( ) represent the trig functions. Also the mapping error includes errors in measuring the location 

of the PBM on both the map and the film. 

Since the vehicle yaw and pitch are always programmed to be zero, '" and e are the yaw and pitch 

errors. Also A X is the mirror stereo position error since X is the calibrated mirror position. The 

error in the mirror crab position has been included in the roll error as a first approximation. Thus the 

computed miss distances (J and (J along with the programmed obliquity angle D , and the calibrated x y 

mirror stereo angle X are known. For the purpose of this analysis the bench mark height will be 

considered as known when computing (J and (J and will be allowed as an error included in (J and (J 

x y xo yo 

The task then is to determine the unknown errors (J ,(J , AX, cP, 6 and '" which cause the miss 

xo yo 

distances (J and (J • 

x Y 

b. Single Frame Case 

Due to the nature of the GAMBIT system the program was formulated so that the 

programmed knowns do not vary over the length of the frame. Also the unknown errors are constant for 

each frame. In reality only the camera orientation errors are likely to be constant over a frame. Since 

the attitude and ephemeris errors are slowly varying during a typical short frame the assumption that 

these errors are constant is reasonable. However, while the error in the map itself may be nearly 

constant over a short frame the errors in measuring the PBM position on both the film and the map may I vary considerably. Hopefully, these measurement errors are somewhat random with a bias nearly equal 

to the probable map error. Since the film and map measurement errors are included in the map error the 

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assumption that the map error is constant during the time of a frame is likely to be poor depending upon 

the randomness of the measurements. Since the map errors are not truly constant during the time of the 

frame, the miss distances calculated from the functional relation (J = f ( ) will not be the same for each 

bench mark in the frame. 

Regarding map and ephemeris errors as a single error, equations 1 and 2 are two equations I in six unknowns. Since this is an undetermined and consequently unsolvable set of equations valid for each 

bench mark in the frame, choice of several bench marks allows the set to be expanded. Choosing three or 

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more bench marks per frame one would expect the resulting set of equations to be exactly or overdetermined 

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Approved for Release: 2018/09/11 C051 03025 

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Approved ~ for Release: 2018/09/11 C051 03025 ,.""...r......I'\,..,f .... "......., ... - '\,.,A,cAJ.'f.l.L..I.I. ... 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

and solvable by the least squares technique. Since the coefficients of the unknowns as well as the unknowns I are considered constant for each bench mark in a frame, equations 1 and 2 may be written 

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(la) 

(2a) 

where the subscript i refers to the i th bench mark in a frame and the trig coefficients have been replaced 

for simplicity. The above equations are 2i equations in six unknowns. However, the right-hand side of 

the 2 i equations is constant for all bench marks (all values of i) so that it is not possible to uniquely 

determine the six unknown errors. Thus choosing any two uncorrelated errors and assuming the other 

errors are zero, a solution is possible. However, neglecting four of the six errors will result, in 

general, in erroneous values for the two determined errors. It should be noted that choosing two 

uncorrelated errors and applying the least squares technique to the 2 i (i > 1) equations the technique 

simply averages over all the bench marks. 

Again any two uncorrelated errors may be determined; however, the determined errors will, 

in general, be erroneous. By picking three sets of two uncorrelated errors and making three runs with 

the program all six errors may be determined. However, all six will be erroneous since they were taken 

two at a time. Nevertheless since only two errors can be determined at a time, the TEAR program has 

been used to determine each set of errors independently of the other sets in order to determine approximate 

values for the errors. 

Since the ephemeris error is slowly varying, neglecting this error and solving for attitude 

error will result in a near constant attitude error bias from frame to frame. Also for the same mirror 

pOSition the error is generally the same so that mirror position error will also introduce a bias into the 

attitude error deter mination. However, in this case the bias will depend upon the position of the stereo 

mirror. Therefore, if the map error is also constant from frame to frame, neglecting all but the attitude 

errors will only bias the results and the relative attitude time history will be meaningful. The map error 

is considered constant over a frame even though this may be an erroneous assumption. Thus the program I is used, on a frame baSiS, to determine two attitude errors ignoring map, ephemeris and camera errors. 

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In other words, in the current usage of the program to determine attitude errors on a frame baSiS, .d I 

(J and (J have been regarded as being equal to zero. The results then, at best, will be an average and xo yo 

only the relative attitude errors from frame to frame will be meaningful. Realizing the above limitations, 

then consistent with the method of using the TEAR program namely neglecting mirror, map and ephemeris 

errors, equations 1 and 2 may be written 

(J = IV tan 9 + e (1 + tan

2 

I 

x cos2 g 

tan I sin g ) + <P cos2 9 

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Approved for Release: 2018/09/11 C051 03025 

(3 ) 

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~ 

for Release: 2018/09/11 C051 03025 t-I.&....I'\J..L ... .&....I A. - '-A..c:I.J.Y..LA.J.I....I. 

BCS 39739-65 

Handle via Byeman 

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PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

tan]; sin Q - 9 cos2 Q 

to show the attitude error dependence. 

(4) 

Examination of equations 3 and 4 show the three attitude errors of which only two can be 

determined on a frame basis. Proceeding blindly and solving for the three errors, two at a time will give 

errOneous results since each solution ignores one of the errors. However, there are certain special 

combinations of the mirror and obliquity angles which allow an accurate solution for at least one of the 

unknown errors. Therefore, certain special cases will be examined where when solving for two of the 

errors, the resulting solution for at least one of the two errors will be accurate. Of course, while 

equations 3 and 4 may be used to determine an accurate solution for one or more of the unknowns the 

accuracy of the determination is still subject to the assumption that 

Case A Strip Vertical ( ]; =: D.]; = a =: 0) o 

a =: O. o 

Considering first the case where ]; == 0, equations 3 and 4 reduce to 

a = 111 tan Q + e 

x 

ay=-q> 1 

cos2 Q 

Thus the roll error may be determined. 

Case B Zero Obliquity ( Q = D.]; = a =: 0) o 

For ]; " 0 and at zero obliquity angle, equations 3 and 4 reduce to 

a = 9 (1 + tan2 ]; x 

a = I/.! tan ]; - fP 

y 

Thus the pitch error can be determined. 

Case C Nadir ( ]; = Q = D.]; == a = 0) o 

At zero obliquity and stereo angles, the equations become 

a = e 

x 

ay=-q> 

so that both the roll and pitch errors can be determined. 

c. Multiple Frame Case 

(5) 

(6) 

(7) 

(8) 

(9) 

(10) 

Since the program formulation assumes the unknown errors to be constant over any 

solution interval, equations la and 2a may be written 

a

j

. Xl 

j a. Yl 

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a

j 

+ xo 

a j 

+ 

yo 

I/.! Aj 

+ e Bj + q> Cj + D.]; Dj 

I/.! Ej 

+ e Fj 

+ q> Gj 

"TOP ~r:CRET - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

(lb) 

(2b) 

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Approved for Release: 2018/09/11 C051 03025 ~""'.a....I"""'..L"'.a....I.L - '-o.A4..L.L .. ..L.LJ ....... 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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where the superscript j refers to the j th frame in the interval of frames where the errors are to be I determined. In general, the coefficients Aj - - - ai will be different for each frame since the programmed 

knowns generally change from frame to frame. The assumption that the ephemeris and mirror errors are 

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constant is reasonable over a few frames since the ephemeris error is slowly varying and the mirror is a 

mechanical system for which the error in position is approximately the same ea ch time the mirror is in 

the same position. While it is likely that the map errors over several frames will vary even more than 

previously discussed, there is some probability that the measurement errors are somewhat random with 

a bias equal to the probable map error. Most critical is the assumption of constant attitude errors since 

an accurate time history (frame to frame) of these errors is desired. The assumption of constant attitude 

errors is poor due to attitude changes caused by the attitude control system instability, the vehicle roll 

maneuvers, changes in the mirror position and other mechanical devices. Considering these attitude 

errors constant over several frames results in the program determining an average error and the detailed 

time history is lost. 

Equations 1b and 2b are 2 i x j equations in six unknowns and solution via the least squares 

technique is indicated. Since for a particular frame (j constant) and for various values of i the equations 

are the same as section b with respect to the averaging property only i constant and various values of j 

will be considered in this section. In particular for j ~ 3 the set of equations is exactly or overdetermined 

and solution is accomplished by the least squares technique. Two factors influence the solution for j ~ 3. 

First the solution may be ill conditioned due to the way the coefficients of equations 1 and 2 vary from 

frame to frame and due to correlation between the unknowns. Secondly, since the program formulation 

assumes the errors to be constant over the j ~ 3 frames, any error which can be determined will be an 

average error over the j ~ 3 frames. 

To examine the correlation between the various unknown errors would require explicit 

expressions for the three map, two film measurement, three ephemeris, mirror stereo, mirror crab, 

three attitude and time errors. Thus including all the errors the correlation would be determined by 

examination of the determinent of a 14 x 14 matrix. Even ignoring all errors except the attitude errors 

the examination of the 3 x 3 matrix would involve at least the coefficients of equations 3 and 4 for two 

frames (j 0= 2). This is an extremely difficult task and, in general, is best handled by using the program 

with several test cases. Also it should be noted that the program had not been used for j ~ 2 and the only I multiple frame case which had been used is the rather special case of stereo pairs. 

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The one case that can be examined in detail where only mirror stereo position and attitude 

errors are considered is the special case of stereo pairs. For stereo pairs the parameters corresponding 

to the first frame of the pair will be denoted with a plus superscript and the parameters corresponding to 

the second frame with a minus superscript. Letting E t and E ~ be the calibrated stereo mirror angles, 

then consider E to be an average value defined by 

Eo=l/2(E+ 

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- E -) 

c 

~-GAMBIT 57 

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Approved for Release: 2018/09/11 C051 03025 

~"""""""''''''''''''''''''''''''''''''.A.'''.J.''''''''''''''''..L 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

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Since the calibrated value is not the true mirror stereo position, the true values are then given by 

I+ = I + ~I+ 

Assuming that ~ I + and ~ I - are small so that 

tan I + = tan I 

tan I - == -tan I 

cos2 I + :: cos2 I 

cos2 I - = cos2 I 

and til, e ," and SJ are constant and equal for both frames of a stereo pair, then equations 1 and 2 for a 

stereo pair with (J :: (J = 0 may be written as 

xo yo 

+ 

(J - (J 

x x 

2 

1/1 tan SJ + e (1 + tan 2 I 

cos

2 SJ 

tan I 

1/1 cos SJ 

tan I sin SJ - e -------"--

= " tan I sin SJ 

cos

2 SJ 

= _,, __ 1_ 

cos2 SJ 

cos

2 SJ 

+ 2 

(11) 

(12) 

1 

cos

2 I cos SJ (13) 

(14) 

where the (J'S refer to the same bench mark in each frame. In this analysis the equations for each frame 

were combined to represent a stereo pair. The TEAR program, for stereo pairs, combines the two sets 

of 2 equations per bench mark per frame into a single set which is twice as large. While this analysis 

differs from the program formulation, conclusions regarding permissible solutions due to the correlation 

of variables will be the same. 

Examination of equations 11 - 14 shows four equations in five unknowns so that it is not 

possible to determine a unique solution for the unknown errors. However, if ~I + and ~ I- are known 

or are zero then examination of the determinent of the 3 x 3 coefficient matrix shows that a unique solution 

can be determined. It should be noted that in the method of using the TEAR program it is assumed that 

~ I + == ~ I - '" 0 so that a unique solution, which is erroneous can be determined. The solution is 

erroneous since the effect of mirror stereo position is ignored whereas this error makes an important 

contribution to equations 11 and 13. Of course, neglecting (J in equations 11 and (J in equation 14 also 

xo yo 

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Controls Only ~GAMBIT Approved for Release: 2018/09/11 C051 03025 

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Approved for Release: --2018/09/11 C051 03025 ~.L:.o'-'~".L:.o J. - Url,lV.lDJ. J. 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

decreases the validity of the solution. 

For zero obliquity the above equations reduce further to 

a+ + a- = 2 8 (1 + tan2 X ) + Ll.X+ + Ll.X- 1 x x 

a+ 

y - a 2 '1/1 tan X 

y 

a+ - a (Ll.X+ - Ll.X-) 1 x x 

cos2 X 

a+ + a = -2 fP 

y y 

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(15) 

(16) 

(17) 

(18) 

Therefore, if Ll.X+ and Ll.X- are known, as before, a unique solution can be determined. Furthermore, 

even if the mirror stereo position errors are not known the yaw and roll errors can still be accurately 

determined. Again in the use of the program Ll.,t+ and Ll.X- are not known and closely coupled with the 

yaw, pitch and roll errors. The coefficient multiplying these terms is large and ignoring these terms 

(i. e., the error in the calibrated mirror position) will generally result in an erroneous determination of 

the attitude errors except yaw and roll at zero obliquity. 

In summary the error in the calibrated mirror stereo position introduces two variables 

which are highly correlated with the attitude errors. Due to this correlation, when using the program, the I mirror stereo error is ignored and the determined attitude errors are erroneous, especially for non-zero 

obliquity angles. For Q =: 0 the yaw and roll error determination is not affected by the mirror errors. 

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However, at larger roll angles even the yaw and roll error determination is further degraded. 

d. Correlation - Multi-Frame Case 

Considering only attitude errors (i. e., a == a xo yo 

written in matrix notation for the j th frame 

Aj 8 = a

j 

where 

[~ . 1 

A

J 

== A11 

8 [ZJ 

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Controls Only 

j 

~\3 ] A12 

j 

A22 A23 

"019 SECRET - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

Ll. X= 0) equations 3 and 4 may be 

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Approved ~ for Release: 2018/09/11 C051 03025 _.&....11_ ....... .&....11.... _ ......... " ... .-....... 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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Controls Only 

and the i subscript referring to the i th PBM in the j th frame has been dropped for convenience. 

For two frames j and k equations 3 and 4 may be written 

[~~] '0 ~] where the total matrices been partitioned. Therefore, the normal equations in the least squares 

process have the coefficient matrix 

with elements 

b 

mn = X X 

j r m, n = 1, 2, 3 

where j is the frame and r is the rows of [A]. Only the triangular matrix is given since B T = B 

(1. e., B is symmetric). Therefore, explicitly the elements are as follows 

X tan D. 

] 

b13 = Xj , [tan X 

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Controls Only 

cos Do 

J 

2 

X [(1 + tan Xj )2 + 

j 

cos2 D 0 

J 

2 2 

tan .t 0 tan Q 0 ] 

J J 

cos2 Q 0 

J 

~GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

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App~rooyvee~d 2QI for Release: 2018/09/11 C051 03025 

~~Cl{~'l' - llAMl:HT 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

[ tan X j tan Il 0 

b = X J 

23 j cos SJ 0 

J 

2 

[tan X j tan 

b33 == X 

j cos2 SJ 0 

] 

(1 + 

SJo 

J 

1 tan2 

+ 

2 

cos

2 cos SJ j 

1 

+ ] 4 

cos Do 

J 

Xo J ) ] 

D. 

J 

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Controls Only 

where the subscript j on the mirror stereo and obliquity angles refer to the j th frame. 

where 

The variance/covariance matrix is given by C == B- 1 so that the correlation is given by 

c 

P pq '" ~===pq~= VC c 

pp qq 

~ 

pq 

v~ ~ pp qq 

~ is the co-factor of b 

pq pq. E~li~~ 

I so that in general it is difficult to derive an analytical e~ression for the correlation. 

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While the correlation is a complex function of the mirror stereo and obliquity angles, 

results can be obtained for multiple frames of the previously discussed special cases. 

Case IA X = 0, 

For multiple frames of X o photography, the correlation is given by 

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o 

~-GAMBIT 

.............. ______________ ..:..A:!::p.!::;pr..:::ov.:.::e:::.:d..:,:fo:::.:.r..:.,R:.:::e.:.:::lease: 2018/09/11 C051 03025 

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Approved for Release: 2018/09/11 C051 03025 ~""".......,,,,,,,.a.,,,.......,.&. """"' ............ .LA...J ........ 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

X tan2 D. 1/2 

-P..",e=[j Xj JJ 

j 

Case IE X 1= 0, D = 0 

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Controls Only 

Since stereo pairs will be considered separately then the only non zero values of X . and 

J 

:£ k will be X. = :£ k . However, the obliquity for this case is zero and for two frames with the same 

obliquity and ~irror stereo angle ~~. = ~~. Therefore, the multiple frames case is exactly 

the same as the single frame case with multiple bench marks. 

Case IC X= 0, X= 0 

It is obvious (Case IB) that multiple frames of nadir photography are exactly the same as 

the single frame case with multiple bench marks. 

Case ID Stereo Pairs 

For a single stereo pair, the correlation is given by 

Pe,,/, = P..",,/, = 0 

Therefore, allowing a correlation of about P.." ,6= . 2 the solution for the yaw and pitch errors will be 

reasonable for -3. 5° ~ D ~ 3.5°. The yaw-pitch correlation is plotted in Figure 1. 

Case IE Xl == X 2 ' D 1 == -D2 

For equal mirror stereo angles along with equal and opposite obliquity angles, the 

correlation is given by 

where 

PI/I,6 =: Pe, cp =: 0 

PI/I,,/,== -tan X 

V b

i 

b

3 

b 2 tan2 l: 1 = tan D + ~~=---

cos2 Q 

b3 = tan2 l: tan2 Q + 1 

2 

po!': Q 

From the yaw-roll correlation plotted in Illustration 19, the correlation is small (Pw, tp ::2 .2) for D ::2 40° . 

Results can also be derived for various combinations of the above cases. 

Case IIA X=:O, D to 0 plus l: = 0, Q =: 0 

P (J , tp == Pcp,"" == 0 

P -1 

!/Fe= -- , ""2 

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PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Case IIB I = 0, Q = 0 plus Q = 0, If, 0 

Case IIC 

where 

Case lID 

I:I:: 0 ,D = 0 plus I =: 0, Q I- 0 

P tjI 8 = - P tan Q 

, V AC 

2 P UlI- (1 + Q ) tan I 

tjI'T - V BC 

Pe,f'; -tan I tanQ 

V AB 

P =: 1 + 1 

cos4 Q 

Q =: (1 + tan2 I ) 

A = P tan2 Q + 

cos4 Q 

B =: Q2 (tan I + tan2 Q ) + tan2 I 

C = (1 + Q2) P 

I=: 0, Q =: 0 plus I I- 0 plus I =:0, Q I- 0 

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For the combination of the three special cases, the correlations are given by the same 

formulas as Case lIC where 

p' P + 1 

Q' Q + 1 

Plots of the correlations are presented in Illustration 20 for Case lID. Case lIC win have the same general 

shape with slightly larger correlations. Note that it is not possible to choose an obliquity angle or range 

of angles for which all three correlations are small. 

Consideration of other combinations of frames is very algebraically complex. However, 

a sufficient but not necessary condition for the correlation to be zero is that the co-factor.6. = O. 

pq 

Several results can be presented utilizing the above condition. I Case rnA Multiple Stereo Pairs 

PtjI,CP '" P8 ,cP =: 0 

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.6.1/r, () = 0 if I tan Q. =: 0 

j } 

Case HIB Stereo Pairs Plus All other Combinations 

The one exception not inCluded in this case is:l::I = I ,Q .. J. Q 

j k J i k 

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PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

I tan Q = 0 

j j 

the correlations are given by 

where 

P""s= 

P8''P = 

PI/I''P= 

2 3 tan Q + 2 

0 

0 

tan X 

.j b

ll 

b

33 

tan2 X 

+ tan2 X 

cos2 Q 

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2 2 

b

33 '" 2 tan ~ tan Q + 3 + 2 

cos Q cos4 Q 

It can be seen from the plot of 

for Q ? 10° 

P"" 'P in Illustration 21 that the roll-yaw correlation is small ( P t/I,'P s:.2) 

While including all combinations is too algebraically complex for analytical analysis, it is 

interesting to investigate what combinations are permissible when requiring zero correlation. Since b

ll 

b22 and b33 cannot be zero except for bll which is zero for the trivial case of X = Q = 0 then for zero 

correlation it is necessary that b12 = b13 = b23 = 0 or 

}: tan Q,= 0 

j J 

tan }:j 

}: 0 

j cos Q, 

J 

tan }:, tan Q j tan2 }: j 

}: J [1 + + 

j cos Q j cos2 Q j 

1 

---] == 0 cos2 Q j 

It does not appear likely that for several randomly chosen frames that the above three 

conditions would be satisfied. Also for several frames of photography the number of variables Q . and X . J J 

greatly exceeds the number of constraining equations. However, from the following table 

L=OQ=O 

L=OQ*O 

L*OQ=O 

L 1 =-X2,Ql=Q2 

L 1 =}:2,Ql=-Q2 

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2 

b

12 b13 

0 0 

tan Q 0 

0 tan }: 

tan Q 0 

tan }: tan}: tan Q 0 2-- 2 cos Q cos Q 

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b

23 

0 

0 

0 

0 

tan2 }: 1 [1 + + cos2 Q cos2 ] 

Q 

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it is obvious that considering multiple frames of stereo and }; 

then all correlations will be zero. 

o photography such that }; tan Q . == 0 

J 

e. Effect of Non-Zero Mirror, Map and Ephemeris Errors 

The effect of an error in the calibrated mirror stereo position is shown in the following 

chart where the indicated attitude errors are coupled to the mirror stereo position error. 

Therefore, some errors are not affected by a mirror stereo position error for different combinations of 

}; and Q. 

The effect of nOn-zero map and ephemeris errors can be determined by replacing (J by 

(J- (J o. Examination of equations 5 - 10 shows the coupling between the attitude and ephemeris errors. 

The components which are coupled depend upon the obliquity angle as shown by the following chart. 

Error 

() 

For stereo pairs it has been assumed that (J~' (J ~ and of course the bench mark is common to both 

frames. Note from the chart that using stereo pairs at zero obliquity the yaw error can be determined 

even for non-zero map and ephemeris errors. However, in actuality (J ~ '" (J 0 and even the yaw error 

determination will be degraded. 

£. Test Case Results 

Prior to the appropriate equations being available for analysis, several test cases were 

designed to help determine how to use the program. Initially, these test cases were designed with zero 

ephemeris error and such that for each bench mark (J == (J == O. Then inputting attitude errors the 

x y 

question was whether or not the solution for attitude errors would be identical to the errors that were 

input. Without exception the results of the previous analysis were confirmed by the test cases. 

* Yaw cannot be determined. 

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Since the actual data is carefully edited to remove obvious errors, data noise (random 

map reading error) was simulated by introducing a small error such that on an individual frame and bench 

mark basis a x and a y were not zero while the average a x and a y per frame were zero. The addition of 

the data noise did not seriously affect the determination of the attitude errors. 

The effect of non-zero values for a xo and a yo was simulated by introducing a data bias, 

i. e., for each bench mark ax and ay on a frame basis are non-zero and equal. The test case results, as 

anticipated, showed that generally the effect of ephemeris and/or map errors degraded the determination 

of the attitude errors. In fact these errors combined to either increase or decrease the attitude errors 

depending upon the sign of the data bias, i. e., axo and a yo and the magnitude of the obliquity angle. In 

particular, the correlations between a xo and @ along with a yo and 'P were very high. 

g. Summary 

(1) The TEAR program can be used post flight, prior to the availability of stellar photography, 

to attempt to determine gross SUb-system malfunctions. Any attempt to utilize the program without 

inputs from the stellar reduction to detect small, nominal, within spec subsystem errors may be 

misleading. In particular, the program should be used first to determine the in-track and cross-track 

ephemeris errors independent of attitude errors. Secondly, the attitude errors should be determined 

independent of ephemeris errors. When solving for the attitude errors on a frame basis, the special 

cases should be used to determine the errors. The attitude errors should only be used to examine the 

relative behavior between adjacent frames or pairs. However, even this use of the program may be 

misleading due to the possible compensating effect of the various errors. 

(2) The following table indicates what combinations are permissible when solving for attitude 

errors in the presence of other system errors and when the other system errors are not so large so as 

to be overriding. 

No Yes Yes No Yes* Yes 

No Yes No No Yes* No 

Pairs Yes Yes Yes No Yes* Yes 

The asterisk indicates serious degradation of accuracy at large obliquity angles. 

(3) An error in the calibrated stereo mirror position (i. e., true pOSition not equal to calibrated 

position) will add an additional unknown d ~ term to the a x equation for ~ = 0 and ~ '* O. For stereo 

pairs an additional unknown term involving d~ + and d ~ - will be added to the two equatiOns in a+ and 

x 

(j. The necessity of neglecting these terms due to the usage of the program will degrade any attitude 

x 

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error determination resulting from a a equation depending upon the obliquity angle. x 

(4) Since a should appear in the a x equation and a in the a equation, all results except xo yo y 

'" from stereo pairs with Q = 0 will be seriously degraded by the necessity of neglecting these terms. 

The degree that the results will be degraded is dependent upon the value of the obliquity angle. 

(5) Since pitch and roll error are so closely correlated with mirror position error (crab and 

stereo) solving for attitude error while neglecting mirror position error will also indicate gross malfunctions in the mirror and/or attitude control system. One way of deciding which system is malfunctioning 

is to observe some pattern which shows the mirror malfunction in a particular position. 

(6) Utilizing the attitude orientation information obtained from the reduction of stellar 

photography, the TEAR program can be used to attempt to determine the ephemeris errors both in the I best fit and command ephemerides. Since the BFE errors are slowly varying over a payload operating 

span, a very limited amount of attitude orientation data derived from the stellar photography will serve 

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to determine the ephemeris errors. Inputting the ephemeris errors will then allow for solution of the 

attitude errors on a per frame and/or stereo pair basis with the same limitations as discussed in the 

analysis. Possible problems may occur due to map and instrument errors along with the correlation 

between the radial, cross-track and in-track ephemeris errors. 

4. Accuracy I The accuracy of the miss distance calculation is largely dependent upon the accuracy of the 

photo map match, i. e., the accuracy of determining the map coordinates of the PBM. In order to 

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determine the influence of map errors and human errors in reading the map, the following analysis was 

conducted. 

Denoting the map coordinates of the intersection of the traced ray with the earth as the computed 

position and the map coordinates of the PBM as the actual position, the coordinate system as shown below 

can be establiShed with the origin at the computed position. 

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N 

Flight Path 

w-r----- -------E 

S 

~-GAMBIT 

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Thus x is the longitude of the actual point relative {actual-computed} to the computed point and y is the 

latitude of the actual point relative to the computed point. Az is the azimuth given by 

A = sin- 1 z ~1 cos¥, 

where i is the orbit inclination and ¥' is the geocentric latitude of the computed point. Also, for convenience 

8= Az - 180° 

Therefore the latitude and longitude of the actual point are related to a x and (Jy by 

so that 

[ ~;] = [~~:: - ~~::] [-;] 

Therefore, an error in the map or in measuring x and y will be reflected in (J x and (J y according to 

c~S e -sin 8] [- 6 Y] 

smB cosB 6x 

which shows the dependence upon the azimuth and consequently the inclination of the orbit and the latitude 

of the computed point. 

For polar orbits, and north to south camera operation 

- 6y = -.15 NM 

6 x = .15 NM 

for typical map and measurement errors of .15 NM. For an orbit inclination of 105° and at approximately 

60° north latitude, B ~ 26.8° so that 

6a x ~ -.2 NM 

flay ~ .07 NM 

which shows that for this particular orbit and latitude the error in the a x and/or (Jy determination can be 

larger or smaller than the error in the latitude and/or longitude measurement. 

5. Method of Making TEAR Runs 

For the PBM's that were chosen the corresponding latitude, longitude, time and film 

measurement along with the appropriate satellite vehicle positions were input to the TEAR Computer 

Program. 

a. USing the BFE satellite position, the a x and (Jy for each individual PBM was determined 

and then edited by comparison with the average a x and a y for the entire frame. A comparison was also I made of the a x and a y of neighboring PBM's. All PBM's whose (J x and (J y were not in close agreement 

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were identified and rechecks of all the PBM parameters were then made. A second computer run was 

then inade with the corrected PBM's to check for agreement with surrounding points. At this point all 

bench marks that did not agree within 2" 0.3 nautical miles with surrounding points were eliminated from I further analysis. Also, all frames with only one bench mark per frame were excluded from further 

consideration. 

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b. The miss distances (o-x and o-y) shown on Geo-Positioning Data Sheets, Appendix A, were 

computed for each individual bench mark using the BFE satellite position, and then averaged for the entire 

photographic frame. Regarding the PBM map position coordinates as the actual position and the coordinates 

of the traced ray as the predicted position, then 0-x is positive if the actual position is south of the predicted 

position and o-y is positive if the actual position is east of the computed position. The Mean Error (ME) 

shown is also computed for each frame. 

c. Due to limitations posed by the correlation between the yaw, pitch and roll error subcomponents the following procedure was used when determining the attitude errors: 

(1) For photography where }; = 0 and the roll angle is zero, the total system error was 

conSidered to be due to attitude error and the attitude error was resolved into pitch and roll components 

without any loss of accuracy even in the presence of yaw. The accuracy of the determined pitch error is 

degraded at greater roll angles. 

(2) For frames where }; '" 0, and for zero roll angle again the total system error was 

conSidered to be caused by attitude error. However, only the pitch component of the attitude error could 

be determined with reasonable accuracy. The pitch error determination is even less accurate for greater 

roll angles. 

(3) For stereo pairs, again the total system error was considered to be caused by attitude 

error and the attitude error was resolved into pitch and roll components. For zero roll angle the yaw pitch 

and roll errors are accurate. The accuracy of the yaw and pitch error determination is degraded for 

greater roll angles. 

d. In Case I the vehicle attitude errors were computed using the BFE satellite position. The 

results of this run are shown on the Data Sheets. In this case the system error is considered to be due 

entirely to attitude errors and is determined as outlined in Section 4. c. 

e. In Case IT the BFE errors were computed using the BFE satellite position. Errors shown 

on the Geo-Positioning Data Sheets under BFE Ephemeris Error columns are the in-track and cross-track 

errors that Would result if all of the system error was caused entirely by the BFE errors. 

£. In Case ITI the command ephemeris errors were computed USing the command ephemeris 

satellite pOSition. The errors in the command ephemeriS are shown on the Geo-Positioning Data Sheets in 

terms of in-track and cross-track errors. This TEAR run used the commanded satellite vehicle position 

for comparison with the bench mark positions. The results shown here give the error that would result if 

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all the system error was caused entirely by command ephemeris errors. Also shown is the difference 

between the command and best fit ephemerides where the sign convention of section g was utilized to show 

which difference is larger in absolute value. 

g. The command and best fit ephemeris errors along with the mean error were averaged 

over each payload operating span on each rev and are displayed on the summation chart (page 87). This 

chart shows the in-track and cross-track error history for each ephemeris. In theory, the errors in the 

BFE should be less than the errors in the command ephemeris since no extrapolation is involved, the 

length of the fit span (tracking data interval) is longer, and the orbit determination is accomplished post 

flight in a more precise manner. These BFE and command ephemeris in-track and cross-track errors, 

along with the mean error, were differenced on the same summary chart. Since both the BFE and command I ephemeriS error determination used the same BM's and the same values for attitude, then the differences 

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in the err~rs must be a slowly varying function. Examination of the differences show the trend to be the 

expected slowly varying function with some dispersion about this trend. This dispersion or noise is due 

to inaccuracy in the rr and rr , the in-track and the cross-track error determination. In other words, the x y 

difference between the true best fit and command ephemeris errors is a slowly varying function and an 

err~r in the determined ephemeriS errors will result in the observed noise. The sign following the error 

number in the difference columns shows which ephemeris had the bigger error in accordance with the 

folIo wing sign convention. 

_ [E'CMD] > 

+ E [EBFE] > 

h. The last several GAMBIT missions indicated in some instances that the miss distances and 

consequently the ep.l:J.emerts errors were, in magnitude, larger for the best fit than the command ephemeriS. 

It has previously been pointed out that the ephemeris errors for either the command or best fit ephemeris 

result from resolving the total miss distances into only ephemeris errors. Also the attitude errors result I from resolving the BFE total miss distances into only attitude errors. Thus, neither the attitude or 

ephemeriS errors are correct. The following example will show that due to this method of using the TEAR 

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program, it is not possible to determine which ephemeris has the larger errors. Consider the BFE to be 

absolutely correct (i. e., no ephemeriS errors) and no map errors so that the miss distances are due to 

attitude or mirror position errors. More speCifically assume the vehicle to have only a pitch error 

corresponding to a finite rr x and a negligible rr y' Now the TEAR program normally is used to determine 

the ephemeriS error due to rr x' resulting in an in-track p approximately equal to rr x even though the I BFE was not in error. Now consider the command ephemeris pOSition to be behind the BFE poSition by a 

distance - p. Then solving for the command in-track ephemeris error would give a rr x :::: 0 and a zero 

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ephemeriS error. Thus, the TEAR results would show the BFE to be in error by p and the command 

ephemeriS to have zero errOr. Also if the command ephemeris were ahead of the BFE by a distance p 

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PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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then solving for the command in-track ephemeris error would give 2ax and 2 p ephemeris error. Due 

to the method of producing the BFE and since the command ephemeris is predicted, the conclusion may be 

drawn that the BFE errors must be smaller than the command ephemeris errors. Also the ephemeris 

errors as well as the difference between the command and best fit ephemeris errors is a slowly varying 

function. Thus, if the TEAR produced results show the BFE ephemeris errors to be larger than the 

command ephemeris errors, the true error must be an attitude, mirror or map error which, in fact, 

compensated for part of the command ephemeris error. Since accurate maps are used the contribution 

due to map errors should be small. Also, since the BFE is more accurate, then true attitude errors 

will tend to increase ax and a y when using the BFE satellite position. Conversely, since the command 

ephemeris is less accurate, then the attitude errors will tend to be more compensating, thus sometimes 

reducing the a x and a y when using the commanded vehicle position. Therefore, if the vehicle has attitude 

errors it is not surprising the BFE ephemeris errors will sometimes appear to be larger than the command 

ephemeris errors. 

i. As mentioned previously for stereo pairs with the absolute value of obliquity less than 

about 3.5 deg the yaw, pitch and roll errors may be accurately determined. 

Frames Yaw Pitch Roll 

7 18 & 19 .636 .599 -.069 

10 11 & 12 .540 .395 -.410 

21 5 & 6 .721 .486 .071 

26 10 & 11 . .047 .042 

= 

-.343 

26 16 & 17 .369 .244 ! -.149 

31 4 & 5 -.138 .325 -.153 

42 28 & 29 .612 .194 -.307 

8&9 .516 .105 -.569 

~ 20 & 21 .046 .025 -.460 

58 4 & 5 .356 .382 -.102 

j. For certain revs the various correlations between the attitude subcomponent errors were 

small so that the yaw pitch and roll errors could be determined on a rev basis as shown below. 

Rev 

5 

24 

27 

32 

37 

58 

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Yaw Pitch Roll 

.400 .294 -.272 

.497 .143 -.356 

.086 -.244 -.387 

.720 -.009 -.344 

.499 .403 -.236 

-.042 .387 -.368 

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k. Based on the data for the entire flight the average errors were 

.302 NM 

-.710 NM 

Yaw .286 deg 

Pitch = • 193 deg 

Roll = -. 364 deg 

5. Statistical Analysis 

The in-track and cross-track miss distances were analyzed on a statistical basis. The 

procedure used was to make the usual frequency of occurrence plots, calculate the probability and plot 

the results on "probability paper" (Illustrations 22-27). Referring to Illustrations 22-27 the probability that 

the error (] win be greater than (] 0 can be found by first determining the intersection of (f - (]o and (f + (] 0' 

where (f is the mean error, with the plotted line. Secondly the probability PL (in percent) corresponding 

to cr :::- (] 0 to the left of a is read off the left hand scale. The corresponding probability PH to the right of 

(f is read off the right hand scale. The desired probability is then the positive difference of PL and PRo 

Since the data bias and distribution is a function of the mirror stereo position and the vehicle 

roll angle the analysis was conducted using several combinations of l: and roll. The analysis of the crosstrack errors was accomplished for l: = 0 (Illustration 22) and l: "* 0 (Illustration 23). For the in-track 

errors the break down was the same (..E = 0, Illustration 24); however, it was necessary to consider sub 

cases for l: :t O. Illustration 25 shows :::- }: t- 0 for roll angles between :t 15 degrees. Illustration 26 is 

the same except the roll angle varies between 15 and 45 degrees. Illustration 27 shows the probability plot 

for the roll angle between -15 and -45 degrees. The results (mean and standard deviation) are summarized 

below where the units are NM. 

For (]y 

Mean 

SD 

For (] x 

Mean 

SD 

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}:= 0 

.12 

.49 

l: =0 l:;;!0 

-.6 -.7 

.4 .45 

l:~0 

-150 ............... 15° 15 1 -15°-+--45° 

+}: -l: +}: -l: +}: := -}: 

.2 .45 -.03 .37 .4 1.0 

.6 .6 .5 .6 .8 .9 

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PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

6. Conclusions 

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a. The pitch (and stereo mirror position) error is closely correlated with the in-track 

ephemeris error and consequently a x' Therefore, the pitch error determined independently from 

ephemeris errors is not the actual pitch error but is highly biased by the presence of an actual in-track 

ephemeris error. In other words, while a x is caused principally by an in-track ephemeris error, then 

solving for pitch independently results in a pitch error equivalent to ax and consequently equivalent to the 

in-track ephemeris error. However, over a payload operating span the in-track ephemeris error is a 

slowly varying function so that the difference between the determined pitch error on succeeding frames is 

a meaningful number within the accuracy bounds of the a x and a y determination. The principle 

inaccuracy in the a x and a y deter min ation is due to map errors. 

The pitch error difference between succeeding frames is caused by either a pitch 

attitude error, an error in the stereo mirror position, or latitude errors in reading the maps. Without 

use of attitude data from the stellar camera it is not possible to determine whether this pitch difference 

is caused by the vehicle attitude control system, the map or the position of the stereo mirror. For this 

mission the vehicle telemetry indicated that the attitude control system (Pitch) did not experience any 

large variations. Examining the difference between the determined pitch error on succeeding frames 

tends to confirm a relatively quiet attitude control system. The following exhibited unusual pitch 

behavior when compared to adjacent frames. 

Frame 

8 12 V 

9 22 F 

11 8 F 

24 17 V 

40 14 F 2.0 -26.94 

41 31 F 3.0 -21. 27 

43 20 F 2.5 -8.51 

least for 

b. Since the orbit plane is usually accurately determined, the major contribution to ay, at 

}: = 0 photography, is due to roll and/or crab errors. For }: ~ 0, the major contribution to 

a is due to roll and/or crab errors. Since the best independent estimate of the BFE cross-track 

y 

ephemeris error is about 300 feet, any ay in excess of 300 feet must be due to roll and/or crab errors. 

Therefore, the TEAR results (roll and/or crab errors) for }: = 0 photography give an accurate 

indication of these errors. For :s if. 0, the accuracy of the errors is slightly degraded. However, it 

is not possible to determine which SUb-component is in error without additional inputs. Nevertheless, 

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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

since the cross-track error is small and it is, again, a slowly varying function of time, the relative 

change of (Jy between succeeding frames gives an indication of the roll (or crab) and yaw errors, While 

it is very difficult to separate (J y into a yaw and roll component, a large symmetrical change in (J y 

between two adjacent frames is indicative of a predominant yaw error. 

c, Comparing the in-track and cross-track miss distances on adjacent frames showed 

that the change was very large on the following frames: 

Ll(J Ll(J 

X Y 

Rev Frame Rev Frame ---

5 11 8 10 

6 5 8 11 

9 21 27 14 

11 4 27 15 

11 7 

24 17 

41 30 

43 18 

Note that all the above frames where Ll(Jx is very large are the second frame of a stereo pair, 

d. The in-track and cross-track miss distances for each Bench Mark on the long (100 sec) 

frames were examined in detail. Several plots of (J x and or (J y versus latitude appear as Illustrations 

28 and 29, Since the mirror system remains fixed, the ephemeris errors are slowly varying and high 

accuracy maps were used, therefore, the miss distances reflect variations in the vehicle attitude during 

the frame. Illustration 28 shows a change in pitch near the center of the frame, Illustration 28 shows 

the effect of calculating the crab correction at the frame center, Illustration 29 shows a change in the 

vehicle roll attitude during the frame. 

Handle via Byeman 

Controls Only T~-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

74 
I ~d .L.I"" for .... 

Release: \,..L.I ..... -2018/09/11 '-A~.l.~y.LLJ C051 ........ 03025 Handle via Byeman 

BCS 39739-65 Controls Only 

I PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

I 

I CASE I D 

Stereo Pairs 

I Yaw - Pitch 

I 

I 

.8 

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I .6 

I P.p, , 

I .4 

I 

I .2 

I 11. 25° 22.5° 33.75° 45° 

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ILLUSTRATION 18 

I Handle via Byeman 

~-GAMBIT 75 

Controls Only 

Approved for Release: 2018/09/11 C051 03025 
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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

-.25 

-.5 

p 

-.75 

-1. 

Handle via Byeman 

Controls Only 

CASE IE 

X ==.t D == - D2 1 2, 1 

Yaw - Roll 

~-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

45.0° 

Handle via Byeman 

Controls Only 

ILLUSTRATION 19 

76 
~r 

'T'_.Approved for Release: 2018/09/11 C051 03025 '1 . B 

.:J£.J\.,.,fi£.J J. - U.nlV.lU.l J. __ Hana e VIa yeman 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Controls Only 

CASE IID 

.60 

.45 

.30 

.15 

- .0475 

- .095 

Pe,cp 

-.1425 

-.19 

Handle via Byeman 

Controls Only 

22.5° 

X::::: 0 , .a::::: 0 

X ::::: 0, .0*0 

X * 0, .a::::: 0 

Yaw - Pitch 

Yaw - Roll 

Pitch - Roll 

- . 1375 

- .275 

- .4125 

- .550 

ILLUSTRATION 20 

~T-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

P.p, e 

77 
I BCS 39739-65 

I PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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.26 

.195 

.13 . 

.065 

I Handle via Byeman 

Controls Only 

CASE III 

Stereo Pairs 

X= 0, D= 0 

X * 0, D= 0 

X= 0, D*O 

Yaw - Roll 

X D. = 0 

j J 

~T-GAMBIT 

B 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

Controls Only 

ILLUSTRATION 21 

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Aooroved for Release: 2018/09/11 C051 03025 ~..&. U.J...J,-""..L'I.r.J...J.L - '-A~.!.Y.1.,JJ.L.L 

Be! 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

0.01r-----.-----.-----.-----,-----,------r-----r-----r----~ 

0.1~----+_----+_----+_----~----4_----~----~----_+----~ 

1~----+-----;-----~----_+-----4~----+_----~-----

2~----+_----+_----+_----+-----~----~----~-----

5~----+-----;-----~----_+-----4------+_--~ 

10~----+_----1_----_r----_+----~------+_-----

20~----+_----1_----_r----_+----~------

30~----+-----~----_r----~------

40~----+-----~----_r----~------

50~----+-----~----~------

60~----+-----~----_r----~ 

70~----+-----~-----

80 ~----+----

90 1-----+--------. 

951----

98 

99 

99.8 

99.9 STD DEV = .4 N. Mi ----_+---~----+_--~--_r--_I 

N = 62 

99.99~ ____ ~ ____ ~ ___ ~ ___ ~ ____ ~ ______ ~ ____ ~ ____ ~ ____ ~ 

-1. 6 

Handle via Byeman 

Controls Only 

-1. 4 -1. 2 -1. 0 -.8 -.6 -.4 

N.M. 

~T-GAMBIT Approved for Release: 2018/09/11 C051 03025 

-.2 o +.2 

ILLUSTRATION 22 

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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

0.01r-----.---~r----,--~-,----~----~----~----~------

0.1 

1 

2 

5 

10 

20 

30 

40 

50 

60 

70 

80 

90 

95 

98 N == 241 

99 

99.8 

99.9 

99.99~ ____ ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ -L~ __ -J 

-2.4 -2.0 

Handle via Byeman 

Controls Only 

-1. 6 -1. 2 -.8 -.4 o +.4 +.8 

N.M. 

C1 y (E:I:,) 

ILLUSTRATION 23 

~GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

80 
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Approved 

~ 

for Release: 2018/09/11 C051 03025 U..L.,,;J"-'.I.\..L.:..I..L - '-.,..II~J,.V~L..I...L.L 

BCS 39739-65 

Handle via Byeman 

Controls Only 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

0.01r-----.------.-----r----~----~r-----~----~-----r-----, 

0.1 ~----+_----4_----~----_+----~~----+_----4_----~----~ 

1 ~----+_----;_----~----_+----~~----+_----4_----_h~ 

2~----+-----4-----~-----+----~~----+-----

5 ~----+_----4_----~----_+----~~----+_-----

10~----+-----4-----~-----+----~~----

20 ~----+_----4_----~----_+----~~----

30 ~----+_----4_----~----_+---~~---

40~----+_----4_----~----_+------

50~----+_----4_----~----_+------

60 ~----+_----4_----~----_+----~~----~----+_----~----~ 

70 f------+_----4_----~-----

80 f------+----+-----~-----

90 f----+----~--

95 ~--+----+-----

98 ~---+-----

991---+--- STD DEV (S) ::: .49 N. Mi __ -+-__ -+-__ -I 

3S = 1. 47 N. Mi 

99.8 ~--

99.91---

99.99 b-____ ~ ____ ~ ____ ~ ____ ~ ____ ~ ______ ~ ____ ~ ____ _L ____ ~ 

-2.0 -1. 6 

Handle via Byeman 

Controls Only 

-1.2 -.8 -.4 0 .4 

(NM) 

(IX (X= 0) 

~T-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

.2 1.2 1.6 

ILLUSTRATION 24 

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Aporoved for Release: 2018/09/11 C051 03025 ~.L...I'-"'.L".L..I""'-'"-"i.4..L41J.a......., ....... 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

0.01r-----r----.r----,----~----~----~----~----~----__ 

0.1r-----~----+_----+_----+_----4_----~----~----~----_J 

1r---~~----+_----+_----+_----4_-----

21----

51-----

101---+---

20f------+-----4-----~-----

301----+-----+-----

401-----+_----+_----

50f----+-----4------

601---+---

70 f-----+----

80 f------+----

901-----

951-----

98 

99 ~---IMEDIAN = + . 2 NM 

STD DEV = • 6 NM 

N = 33 

1----+- E= - 15 

MEDIAN = + • 45 NM 

STD DEV = . 6 NM 

N = 35 

99.8r---~---~----+-----+_----4_--~----~----~----_J 

99.9~----~-~~--_1---_1---_4----_+---_+----_+----~ 

99.99~ ____ L-__ ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ _L ____ ~ 

- 1. 2 

Handle via Byeman 

Controls Only 

-.8 - .4 o .4 .8 1.2 

~-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

1.6 2.0 2.4 

ILLUSTRATION 25 

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Approved for Release: 2018/09/11 C051 03025 ~,"","&''''..L...I..a.-'''''''''.4.A..i.'''''''''''''..B....a. 

BCS 39739-65 

Handle via Byeman 

Controls Only 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

0.01 r-----.-----~----~----,_----,_----~----~----_?----~ 

0.1 ~----~----_r-----+----_4----~~---

1 

2 r-----~----~----~----_4-------

10 ~--+_--

20 1----+----

30 ~---4-----_r-----

40 ~---~--_r---

50 1----+---

60 ~--+_--

70 1----+---

80 f----.... 

901----

95 ~--L_ 

98 

99 

STD DEV = . 50 NM 

N= 35 

----1--E= -15 

N= 40 

99.8 ~---~----_r-----+----_4----~~----+-----4------+----~ 

99.9 ~----4-----_r-----+----_4----~~----+-----~----~----~ 

99.99 ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ ~ ____ -L ____ ~ ____ -J 

-1. 2 -.8 

Handle via Byeman 

Controls Only 

-.4 o .4 .8 1.2 

~-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

1.6 2.0 2.4 

ILLUSTRATION 26 

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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

0.01.---------r-----r------,-------,--------~--------~------~------__ ----__ 

0.1r-----+_----+-----+-----4-----4-----~----~-----+----~ 

1~----+_----+_----+_----~----~--

MEDIAN = + . 4: NM 

STD DEV = . 8 NM 

N = 26 

21---~ 

51----

10 1------+----

20r-----+-----+_----

30~---+_----+----+_----

40 I------+-----~----~-----

50 ~---+_---+_---

60 r----+-----+-----

70 1----+----

80 I----+--~ 

901-----

95 

x = -15 

STD DEV = • 9 N. Mi 

N = 28 

98r---~--~-~~-~---_4----_4----_4----_4----~ 

99 ~--~r_--~----_+----~----+_----+_----~--~~--~ 

99.8r----~--~~--~-----4----_4----_4----_4----_+----~ 

99.9 r----+_----+-----+-----4-----4-----~----~-----+----~ 

99.991--____ ~ ___ ~ ___ ~ ____ ~ ____ ~ ____ ~ ____ _L ____ _L ____ ~ 

-1.2 -.8 

Handle via Byeman 

Controls Only 

-.4 o .4 .8 1.2 

-,oIOF ~ECR~'1:. - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

1.6 2.0 2.4 

ILLUSTRATION 27 

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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

-.5 

-.4 (J DIRECTION OF FlJGHT 

-.3 

-.2 

00 

~ SE -.1 

...:I 

~ O~------------­

~ :;:I 

~ .1 

. 2 I-

• • 

• • • 

• • 

• • 

• • • • 

• 

(j vs Lat 

X 

• 

• 

•• 

• 

• • 

• 

42 43 44 45 46 47 

-1. 2 

DEGREES LATITUDE 

(j vs Lat 

y 

-1. 1 (J DffiECTION OF FlIGHT 

-1.0 

00 

~ -.9 

SE 

...:I < -.8 

u 

~ 

:;:1_ 71- < . z 

-.6 I-

-.5 I-

-.4 I-

• 

• • 

• 

42 43 

Handle via Byeman 

Controls Only 

• 

• 

• • •• 

• • 

• • • 

•• 

• 

• 

• • 

• • 

44 45 46 47 

DEGREES LATITUDE 

~GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

• 

• 

Handle via Byeman 

Controls Only 

• • 

• 

• • 

• 

•• 

REV D16 FRAME 002 

I 

48 49 

• 

• • • 

• 

• • • 

REV D16 FRAME 002 

I 

48 49 

ILLUSTRATION 28 

50 

50 

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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

-.8 

• -.7 

• tf.l • • • ~ 

...:l -.6 • S1 • • • 

...:l 

< -.5 • • 

u • ~ 

::> 

< -.4 

z 

• 

• 

• 

-. 3 ~ REV D31 FRAME 006 

-.2 

(J DIRECTION OF FliGHT 

-.1 

30 31 32 

• -1. 0 r • 

• • • 

-.9 l- •• • • 

- -.8 r • tf.l 

~ 

...:l -.7 I- ..... 

::E 

...:l 

< -.6 

u 

..... 

Eo< 

::> < -.5 

z 

-.4 r 

-,3 r 

REV D47 FRAME 007 

-.2 lI I 

36 37 38 39 

(] vs Lat 

Y 

• • • • 

• • 

•• • 

33 34 

DEGREES LATITUDE 

(] VS Lat 

y 

• 

• 

• -• • - • 

• 

I I 

40 41 

DEGREES LATITUDE 

Handle via Byeman 

Controls Only ~-GAMBIT 

• 

• 

(J 

• 

• 

• 

Approved for Release: 2018/09/11 C051 03025 

• 

• 

• 

• 

35 

Handle via Byeman 

Controls Only 

• 

• 

• . 

• 

• 

• 

• 

• 

36 37 

DIRECTION OF FliGHT 

• 

.-

• 

• • •• 

• 

I I 

42 43 

ILLUSTRATION 29 

44 

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Bes 39739-65 

PERFORMANCE EV ALUA TION TEAM 

REPORT NO. 4022/65 

EPHEMERIS COM PAR ISO N 

SUMMARY B Y REV S 

BEST FIT EPHeMERIS COMMAND EPHEMERIS 

I 

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MSG 

NRIO 

103 

]05 

108 

109 

110 

112 

113 

114 

116 

117 

118 

121 

122 

123 

125 

121 

128 

129 

130 

132 

FIT 

SPAN 

01-02 

01-04 

01-06 

01-08 

01-10 

01-14 

06-11 

09-20 

13-23 

15-26 

21-32 

23-34 

25-3A 

29-39 

32-42 

39-50 

41-52 

46-55 

46-55 

48-59 

EPOCH LOAD 

REV REV 

02 04 

04 06 

06 08 

08 10 

10 14 

14 16 

17 19 

20 22 

23 25 

26 30 

32 33 

34 36 

36 38 

39 41 

42 46 

50 52 

52 54 

55 58 

55 59 

59 63 

Handle via Byeman 

Controls Only 

OPS 

REV 

05 

06 

07 

08 

09 

10 

11 

14 

15 

16 

20 

21 

22 

23 

24 

25 

26 

27 

31 

32 

34 

37 

38 

39 

40 

41 

42 

43 

48 

53 

54 

55 

56 

58 

59 

63 

64 

IN-TRACK 

.462 

1.155 

1.295 

.135 

.458 

.538 

.865 

-1.097 

-.137 

.276 

.164 

.599 

.445 

.003 

.2l8 

-.058 

.272 

-.428 

.139 

-.014 

-.289 

.631 

.423 

.355 

.769 

-.059 

.329 

.505 

-.067 

.036 

.592 

.1l3 

-.064 

.414 

.717 

.643 

.. 642 

-.005 

-.146 

X-TRACK 

-.662 

-1.051 

-.058 

-.900 

-.889 

-.622 

-.985 

-1.318 

-.532 

-.139 

-.752 

-.481 

-.870 

-.987 

-.744 

-.576 

-.499 

-.782 

-.462 

-.505 

-.692 

-.511 

-.963 

-.865 

-.873 

-.834 

- .. 624 

-.993 

-.695 

-.699 

-1.114 

-.838 

-.608 

-1.535 

-.585 

-.581 

-.628 

-.959 

-.745 

ME 

.712 

1.189 

.928 

.947 

.846 

.728 

1.108 

1.218 

.597 

.637 

.577 

.686 

.802 

.686 

.875 

.455 

.523 

.770 

.451 

.509 

.539 

.751 

.835 

.715 

.955 

.784 

.660 

1.058 

.524 

.585 

.890 

.141 

.539 

1.233 

.673 

.676 

.701 

.144 

.. 685 

IN-TRACK 

.038 

.265 

-.030 

.056 

-.459 

.252 

.535 

-.529 

.399 

.418 

1.127 

1.145 

1.071 

1.735 

.225 

.685 

.114 

1.331 

.. 444 

1.313 

.671 

.666 

1.160 

-.773 

-.609 

-.698 

.169 

.305 

.293 

.062 

-.144 

.075 

.058 

.109 

-.154 

-1.609 

-2.153 

~-GAMBIT 

___________________ ~A!:!pproved for Release: 2018/09/11 C051 03025 

X-TRACK 

-.632 

-.974 

-.059 

-.825 

-.804 

-.599 

-.869 

-1.377 

-.521 

-.831 

-.809 

-.533 

-.863 

-.985 

-.729 

-.538 

-.462 

-.740 

-.470 

-.506 

-.721 

-.544 

-.995 

-.910 

-.893 

-.856 

-.651 

-1.002 

-.714 

-.725 

-1.013 

-.833 

-.611 

-1.567 

-.652 

-.618 

- .. 682 

-.987 

-.768 

Handle via Byeman 

Controls Only 

EPHEMERIS ERROR 

(COMMAND - 8FEJ 

IN-TRACK 

-.424+ 

- .. 890+ 

-1.325+ 

-.679+ 

-.911-

- .. 286+ 

-.330+ 

-.409-

-.392-

.123-

.254-

.528-

.700-

1.066-

1.511-

.283-

.413-

.. 542+ 

1.192-

1.940-

.133-

.676-

.248-

.311-

.391-

-.714-

-.938-

-1.203-

.. 236-

.269-

- .. 299+ 

-.051+ 

- .. 080-

-.399+ 

- .. 659+ 

-.796+ 

-1.604-

-2.007-

X-TRACK 

.. 030+ 

.077+ 

-.001-

.075+ 

.. 085+ 

.. 023+ 

.116+ 

.001+ 

.Oll+ 

-.092-

-.051-

-.052-

.007+ 

.. 002+ 

.. 015+ 

.. 038+ 

.037+ 

.042+ 

- .. 008-

-.001-

-.029-

-.033-

-.032-

-.045-

- .020-

-.022-

- .. 027-

- .009-

-.019-

-.026-

.041+ 

.. 005+ 

- .. 009-

-.052-

-~067-

-.037-

-.054-

-.028-

-.023-

ME 

-.095 

-.357 

-.658 

-.173 

-.045 

-.089 

-.159 

.192 

.091 

.079 

.088 

.282 

.279 

.321 

.596 

-.001 

.143 

-.076 

.570 

.914 

.065 

.350 

.091 

.122 

.]80 

.175 

.]02 

.048 

.. 022 

.050 

-.099 

-.010 

.014 

- .009 

-.146 

-.118 

.603 

87 
~-GAMBIT Approved for Release: 2018/09/11 C05103025 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

ControlS Unly 

COMPUTED VEHICLE ATTITUDE 

.1 ~L.ulL." •• '~~l'L",_,,-.",uL.hILrr-._c..,-~~ .• -".."-"'~_--"-",..,-

Handle via Byeman 

Controls Only 

=!L-______________________________________________________________________________________________________________________________________ ~ 

Handle via Byeman 

Controls Only ~GAMBIT Handle via Byeman 

Controls Only 

Approved for Release: 2018/09/11 C05103025 

ILLUSTRATION 30 

T~-GAMBIT c op,/ 6" 

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App!.oved !?~R~I~~~ ~018/0~~ ~fQ~ 12.3.925 

- BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

Controls Only 

APPENDIX A 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

Controls Only 
- - - - - - - - - - C05'103025' 

- - - - - - Approved for Release: 2018/09/11 

::r: G E U - P 0 S I T I o N I N G 0 A T A !:tI ~ !:XI jl.l trj () () ;:l PHOTO COMMANDED MAP toll SS DISTANCE ATTITUOE ERRORS EPHE;4E, I S ERRORS "d ::tl I:I.l 0 Q.. 

0 "zj CA) g. ....... 1 .. 0. POSITION ACCURACY NAUTICAL MILES DEGREE S NAUTICAL MILES !:tI 0 <.0 ('I) 

'"'l !:tI -l '"i <: BES T FIT COMMAND CA) COt-1M AND - BFE 

~ <.0 0 ...... Z I ....... jl.l Ul REV FRAl4E ROLL CRAB STEREO +/- FEET SIG X S I G Y ME PITCH ROLL IN-TRACK X-TRACK IN-TRACK X-TRACK IN-TRACK X-TRACK 0 0) 

OIJj Z CJ1 -24.81 2.0 2F 1600. .296 -.878 .658 .116 .293 -.903 -.189 -.841 - .. 482+ .062+ Il'> () ;:l ~ 9 19.85 2.5 2F 1500. .098 -.622 .454 .104 .107 -.636 -.367 -.690 -.474- -.054- 0 trj ...... ('1) 0 10 36.15 2.5 2F 1280. .864 -.677 .780 .602 .899 -.678 .412 -.792 - .. 487+ -0114- N ~ 8 D II 36.15 2.5 2A 1280. 1.710 -. 002 1.210 1.050 1.752 trj .031 1.381 -.091 -.371+ -.122- N 

~ 

~ jl.l 10-11 STEREO PAIR 1280. 1.287 -.339 1.018 .671 -.148 1.325 -.324 .896 - .. 442 -.429+ -.118- 0) ;:l 12 -15.59 2.5 2F 1300. .195 -.769 .563 .085 .195 -.791 -.267 -.749 -.462- .042+ a CJ1 13 -15.59 2.5 2A 1300. .602 -.425 .524 .389 .614 - .. 439 .247 -.399 -.367+ .040+ t"" D 12-13 STEREO PAl R 1300. ,398 -.597 .. 544 .248 -.364 .405 -.615 -.010 -.574 - .415+ .. 0&"1+ 

~ D 14 -43.95 1.5 2F 1200. -.165 -.909 .660 -.216 -.187 -.931 -.642 -.763 -.455- .168+ 0 15 -43.95 1.5 2A 1200. .160 -.845 .613 .184 .H9 -.869 -.182 -.701 -.331- .. 168+ D 14-15 STEREO PA IR 1200. .025 -.872 .633 .015 '"'l -.289 .009 -.895 -.373 -.727 -.382- .. 168+ .... D 45.37 2.0 2F 0 900. .368 -1.758 1.276 .462 .442 -1.779 -.415 -1.619 - .. 857+ .160+ a 45.31 2.0 2A 900. 1.698 -1.347 1.536 Z .886 1.791 -10313 .860 -1.151 -.931+ .. 156+ 0 4- 5 STEREO PAIR 900. 1.033 -1.553 1.412 .470 -.444 1.116 -1.547 .222 -1.389 -.8'14+ .. 158+ '"'l 0 15 31.90 2.5 2V 1300. 1.162 -.462 .887 .787 -.207 1.194 -.468 .291 -.470 - .897+ -.002- trj 16 31.90 2.5 2V 1120. 1.159 -.612 .938 .787 -.274 1.191 -.623 .316 -.633 -.875+ -.010- > a 18 .00 3.5 2F 900. .796 -.328 .610 .501 .816 -0339 -.553 -,306 -1.3609+ 11033+ is: 0 19 • 00 3.5 2A 900 • 1.251 oll6 .890 .785 1.282 0120 -.026 .150 -1.308+ .030- 0 18-19 STEREO PAIR 900. 1.023 -.106 .763 .637 -.071 1.049 -.108 -.289 -.076 -1.338+ .032+ 0 20 20.56 3.5 IF 900. 1.329 .013 .941 .815 1.363 .015 .003 -.015 -1 .. 360+ - .. 030+ a 21 20.56 3.5 lA 900. 1.666 -.046 1.179 1.022 1.709 -.045 .. 448 -.079 -1.261+ -.034- 0 20-21 STEREO PAiR 900. 1.482 -.014 1.056 .884 -.023 1.520 -.013 .205 -.044 -1 .. 315+ -.031-

a 8 10 -29.06 2.0 2F 1375. .918 -1.551 1.216 .432 .920 -1.601 .310 -1.599 -.610+ .002+ D 8 11 -29.06 2.0 2A 1380. .607 -1.293 1.013 .455 .605 -1.333 -.016 -1.329 - .. 681+ .. 004+ 0 B 10-1I STEREO PAIR 1378. .745 -1.408 1.137 .448 -.150 .745 -1.452 .095 -1.449 -.650+ .. 003+ D 8 12 39.70 2.0 2V 600. -.471 -.217 .377 - .. 310 -.086 -.479 -.232 -1 .. 156 - .. 079 - .. 6-'-(- .. 153+ a 8 13 22.68 2.5 2A 1900. .508 -.602 .559 .279 .526 -.613 -.195 -.50~ -.721+ .109+ D 8 16 11.34 3.0 IF 1I00. .998 -.812 .910 .667 1.026 -.831 .383 -.742 -.643+ .. oa9+ D 8 17 1l.34 3.0 IA 1l00. 1.507 -.790 1.203 .920 1.548 -.803 .813 -. HI -.735+ .092+ 

~ 0 8 16-17 STEREO PAIR 1100. 1.229 -.802 1.053 .772 -.510 1.263 -.818 .578 -.728 -10685+ .. 090+ 

0 17 24.81 2.0 IF 880. -.470 -.917 .730 -.208 -.467 -.944 -1.326 -.836 -.859- .. 108+ 

~ 0 18 24.81 2.0 lA 8~0. .344 -1.189 .f377 .132 .373 -1.210 -.553 -1.098 -.926- 0112+ 

~ 0 9 17-18 STEREO PAIR 860. -.063 -1.053 .807 -.020 -.561 -.047 -1.077 -.939 -.967 -.892- .110+ 

tJj ~ 0 9 19 36.86 1.5 2V 780. .172 -1.231 .881 .131 -.476 .208 -1.254 -.689 -1.108 -.897- .146+ 0 9 20 32.61 2.0 2F 680. .437 -1.112 .853 .379 .471 -1.128 -.401 -.995 -.872+ .133+ b:! H 0 9 21 32.61 2.0 2A 667. 1.426 -1.570 1.50~ .738 1.495 -1.577 .547 -1.440 - .. 948+ .137+ >-3 0 9 20-21 STEREO PAIR 613. .916 -1.362 1.251 .572 -.589 1.029 -1.373 .116 -1.238 -.913+ .135+ 1-1 a 9 22 -24.81 2.0 2F 783. -.009 -1.128 .804 -.086 -.022 -1.156 -.900 -1.H6 -.878- .010+ >-3 D 9 23 -41.83 2.0 2V 700. .784 -1.264 1.054 .496 -.476 .776 -1.313 -.159 -1.352 -.935+ -.039- D 9 24 -14.88 2.5 2F 900. .680 -.522 .612 .400 .695 -.539 -.207 -.504 -.902+ .035+ a 9 25 -14.88 2.5 2A 900. .681 -.519 .610 .439 .696 -.535 -.252 -.501 -.948+ .03~+ 0 9 24-25 STEREO PAiR 900. .681 -.520 .611 .417 -.330 .695 -.537 -.229 -.502 -.91~+ .035+ 0 9 26 14.18 2.5 2A 1300. .915 -.562 .804 .580 1.003 -.570 .047 -.476 - .. 956+ .. 094+ 0 9 27 28.36 2.5 IF 700. -.OlD .040 .039 -.010 -.011 .041 -.923 .165 -.912- .124- 0 9 28 28.36 2.5 lA 700. .274 -.206 .244 0155 .283 -.208 -.101 -.082 -.990- .126+ 0 9 27-28 STEREO PAIR 700. .132 -.083 .174 .091 -.049 .136 -.084 -.815 .041 -.951- .125+ 

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Approved for Release: 2018/09/11 C05103025 
- - - - - - - - -...aIr 

- COs10302S-

- - - - - - Approved for Release: 2018/09/11 

G E 0 - p 0 s ! T I G N I " G D A T A 

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p.:l PHoTO COMMANDeD MAP MISS tr::I (j 01 STANCt ATTITUDE ERRORS EPHEMERIS ERRORS 'i:j (J :::l ::d rn 0 0.. 0 ~ W 1.0. POSITION ACCURACY NAUTI CAL MI LES DEGREES NAUTICAL MILES 

::c @ co ~ ...... -3 ('I) BEST FIT COMMANO COMMAND - BfE 1-3 W '"i <! P ~ co 0 ...... REV FRAME ROLL CRAB STEREO +/- FEET S IG X SIG Y ME PITCH ROll IN-TRACK X-TRACK IN-TRACK X-TRACK IN-TRACK X-TRACK I 

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Z CJI Ul 

to 10 19.14 1.5 2F 760. .447 -1.533 1.130 .359 .506 -1.533 .298 -1.467 - .. 208+ .066+ "" (j 0 10 4 19.14 1.0 2A 760. 1.224 -.620 .972 .663 1.274 -.590 1.0 17 -.523 - .. 257+ .067+ 0 tr::I '<! 0 10 3- 4 STEREO PAIR 760. .835 -1.077 1.054 .. 446 -.557 .890 -1.063 .657 -.997 -.233+ .066+ N :::l ('I) D 10 7 21.27 2.0 IF 800. 1.045 -1.506 1.298 .713 1.109 -1.501 .881 -1.425 -.228+ .076+ N tr::I ....... 

'<! S D 10 8 21.27 2.0 IA 800. 1.842 -.781 1.417 1.027 1.909 -.749 1.641 -.671 -.268+ .078+ "----

p.:l <J) ;;; 0 lD 7- " STEREO PAl R 800. 1.444 -1.144 1.359 .796 -.583 1.509 -1.126 1.261 -1.049 -.248+ .077+ CJI :::l 0 10 9 5.67 2.0 IF 700. .816 -.811 .815 .490 .. 842 -.819 .601 -.770 -.241+ .049+ D 10 10 5.67 2.0 lA 700. 1.231 -.628 .978 t"' .708 1.267 -.632 .985 -.582 - .. 282+ .050+ 

~ 0 10 9-10 STEREO PA IR 700 .. 1.023 -.720 .900 .594 -.441 1.054 -.726 .793 -.676 - .. 261 + .050+ 0 10 11 -5.67 1.5 IF 600. .430 -.897 .705 .239 .438 -.913 .219 -.879 -.219+ .034+ 1-3 0 ID 12 -5.67 1.5 l' 600. .814 -.428 .655 .481 .834 -.439 .541 -.404 - .. 293+ .035+ 

D 

0 10 

10 

11-12 

13 -36.15 

STEREO 

1.5 

PAl R 

2' 

600. 

700. .127 

.622 -.663 

-.492 

.680 

.362 

.364 

.110 

-.412 .636 -.677 .380 -.642 -.256+ .035+ S .115 -.506 -.175 -.527 -.290- -.021- Z 0 10 14 -29.06 1.5 2F 620. .024 -.647 .460 -.043 .010 -.659 -.251 - .665 -.261- -.006- 0 

0 

10 

10 14-15 

15 -29.06 

STEREO 

2.0 

PAIR 

2A 620. .260 -.061 .209 .158 .265 -.068 -.033 -.072 - .. 298+ -.004- 1-3 620. .142 -.354 .357 .099 -.165 .138 -.365 -.142 -.369 -.280- -.004- 0 10 16 -19.14 1.5 2F 600. tr::I -.217 -.729 .542 -.169 -.231 -.741 -.492 -.725 - .261- .016+ D 10 17 -19.14 2.0 2' 525. ;t:- .006 -.149 .115 .010 .005 -.152 -.302 -.136 - .307- .. 016+ 0 10 16-17 STEREO P.IR 554. -.080 -.372 .348 -.032 ;s: -.208 -.086 -.379 -.375 -.363 -.289- .. 016+ 0 10 18 -21.27 2.0 2V 600. -.202 -.619 .463 -.135 -.357 -.215 -.630 -.502 -.615 -.287- .015+ 0 10 19 -24.10 2.0 2V 700. .038 -.646 .460 .019 -.357 .030 -.662 -.256 -.652 -.286- .010+ 0 10 20 -29.77 2.0 2V 700. .129 -.673 .492 .076 -.340 .121 -.691 -.161 -.692 -.282- -.001- 0 10 21 -42.54 2.0 2' 600. .596 -.474 .542 .403 .599 -.501 .262 -.530 -.337+ -.029- 0 10 22 -36.86 1.5 2V 700. .301 -.364 .352 .191 -.169 .301 -.400 .001 -.414 -.300+ -.014- a 10 23 -33.32 2.0 2V 660. .072 -.382 .280 .043 -.179 .068 -.393 -.232 -.400 -.300- -.007- 0 10 24 -42.54 2.0 2' 822. .435 -.912 .727 .350 .425 -.945 .085 -.972 -II 340of- -.027- D 10 25 -29.06 2.0 IF 800. .476 -.827 .677 .220 .477 -.855 .184 -.852 -.293of- .003+ 0 10 26 -29.06 2.0 IA 800. .649 .001 .461 .402 .665 -.008 .324 -.003 -.341+ .005+ 0 10 25-26 STEREO PAIR 800. .562 -.413 .579 .365 -.207 .571 -.431 .254 -.428 -.317of- .003+ 0 10 n 14.88 2.5 IF 600. .983 -.510 .785 .636 1.011 -.516 .729 -.438 -.282of- .078+ 0 10 28 14.88 2.5 l' 600. 1.266 -.035 .897 .786 1.298 -.026 .946 .053 -.352+ .079- 0 10 27-28 STEREO P'IR 600. 1.111 -.294 .838 .669 -.180 1.141 -.293 .828 -.215 - .. 313+ .078+ 

§? D 11 32.61 2.0 IF 900. .197 -1.133 1.239 .302 .267 -1.747 -.003 -1.648 - .. 270of- ..099+ 0 II 4 32.61 2.0 l' 900. 1.099 -1.573 1.360 .528 1.188 -1.557 .848 -1.454 -.340+ .103+ 0 11 3- 4 STEREO PAIR 900. .648 -1.653 1.301 .360 -.672 .727 -1.653 .422 -1.552 - .. 305of- .101+ f; s;: D 11 5 36.86 2.0 IF 700. .533 -1.275 .979 .461 .599 -1.271 .323 -1.157 -.276+ .114+ 0 11 6 36.86 2.0 lA 700. 1.611 -.501 1.194 .900 1.672 - .. 444 1.330 -.329 -.342+ .115+ 

ttl 0 II 5- 6 STEREO PAIR 700. 1.072 -.888 1.092 .512 -.326 10136 -.859 .826 -.745 - .. 310+ .. 114+ 0 11 7 43.24 1.0 2' liDO. 1.838 -.660 1.382 1.016 s;: H 1.915 -.583 1.559 -.450 - .. 356+ .133+ 0 11 8 36.86 2.5 IF 1000. -.295 -1.138 .832 -.041 -.277 -1.172 -.601 -1.048 -.324- .124+ 1-3 0 II 9 36.86 2.5 lA 1000. .450 -.145 tD 0 .345 .263 .465 -.138 .063 -.013 -.402+ .125+ H 11 8- STEREO PAIR 1000. .119 -.586 .611 -.011 -.233 .135 -.598 -.232 -.473 -.367- 0125+ 1-3 0 14 I - 39.70 2.5 IF 500. -1.104 -1.470 1.301 -.848 -1.142 -1.512 -1.532 -1.511 -.390- .001+ 0 14 2 -39.70 2.5 l' 500. -1.019 -1.225 1.129 -.522 -1.052 -1.247 -1.481 -1.245 - .429- .002+ 0 14 1- STEREO PAIR 500. -1.061 -1.347 1.218 -.598 -.554 -1.097 -1.378 -1.506 -1.377 -.409- .001+ 0 15 1 -32.61 2.0 IF 700. -.377 -1.200 .891 -.341 -.406 -1.222 -.769 -1.223 - 0363- -.001- 0 15 2 -32.61 2.0 1A 700. -.249 -.772 .576 -.099 -.267 -.787 -.649 -.787 -.382- .000+ 0 15 1- STEREO PAIR 700. -.313 -.986 .750 -.176 -.474 -.337 -1.005 -.709 -1.005 -.372- .000+ 0 15 3 -43.24 1.5 IF 500. -.1l4 -.676 .486 -.156 -.134 -.690 -.488 -.719 -.354- -.029- D 15 4 -43.24 1.5 l' 500. .270 -.992 .728 .262 .254 -1.023 -.167 -1.049 - .. 421+ -.026- a 15 3- 4 STEREO PAIR 500. .078 -.834 .619 -.001 -.271 .060 -.856 -.328 -.884 -.388- -.028- 0 15 5 -38.99 2.0 IF 760. .151 -.421 .320 .045 .147 -.435 -.221 -.448 -.368- -.013- ::r: 0 15 6 -38.99 2.0 l' 760. .502 .336 .428 .282 .520 .336 .099 .324 - .. 421+ -.012+ 0 15 5- 6 STEREO PAIR 760. .327 -.043 .378 .233 -.008 .334 -.049 -.061 -.062 - .. 395+ -.013- p.J 0 

0 

15 

15 

7 

8 

-1.41 

22.68 

2.5 

2 

2V 400. -.244 -.306 .282 -.164 -.206 -.249 -.315 -.649 -.268 -.400- 11047+ (J :::l .. 5 2V 500. -.253 -.502 .400 -.166 -.212 -.254 -.518 -.652 -.435 -.398- .. 083+ 0 0 0.. 15 9 -.70 3.0 2V 400. -.940 -.788 .887 -.635 -.532 -.962 -.812 -1.366 -.761 -.404- .051+ a ..... 

('I) 0 16 I -6.38 .0 2V 400. .445 -.806 .692 .289 - .. 520 .454 -.825 .592 -.911 .138- -.086- '"i 0 16 2 -1l.34 2.5 2V 400. .055 -.864 .665 <! .033 -.563 .053 -.885 .181 -.976 .128- -.091- 0 ...... 0 16 3 -14.88 2.5 2V 600. .286 -.754 .572 .191 -.484 .289 -.775 .398 -.871 .109- -.096- ...... p.J D 16 4 -24.81 2.5 2F 600. .703 -.952 .842 .377 .713 -.984 .847 -1.088 .134- -.104- Ul 0 16 -25.52 2.5 2' 600. .. 849 -.200 .620 .550 .869 -.211 .974 -.314 .105- -.103- 0 D 16 4- 5 STEREO PAIR ttl 0 16 6 -19.85 2.5 2V 600. .768 -.618 .752 .490 -.350 .782 -.640 .904 -.744 .122- -.104- '<! 400. .311 -.177 .287 .210 -.lIl 0318 -.184 .416 -.284 .098- -.100- :::l ('I) ....... ;t:- O 16 7 -.70 3.0 2V 400. .475 -.355 .420 .322 -.240 .487 -.365 .591 -.450 .104- -.085- I '<! a 0 20 9 -31.90 1.5 2F 1850. .021 -.932 .666 -.072 .004 -.951 .280 -1.009 .276- -.058- N p.J 0 20 10 -31.90 1.5 2A 1933. .376 -.467 .432 .259 .317 -.484 .602 -.542 .225- -.058- :::l 0 20 9-10 STEREO PAIR 1886. .173 -.732 .577 .102 -.347 0164 -.752 .418 -.809 .254- -.057-

Approved for Release: 2018/09/11 COS10302S 
- - - - - - - - - - C0510302S. 

- - - - - - Approved for Release: 2018/09/11 

::r:: G E 0 - P 0 S r T I {) N I N G D A T A 

::0 "0 t;J:l P tr! tr! (') n ::l PHOTO COMMANOED MAP MI5S or STANCE ATTITUOE ERRORS EPHEMERIS ERRURS "0 ::0 fI.l 0 0- 0 I'lj c.:> a ....... 1.0. POSITION ACCURAC Y NAUTICAL >11 LES DEGREES NAUT ICAL MIL ES ::0 @ co (1) 

>oj -l '"i <: BEST fIT COMI'-lAND COMMAND - BFE c.:> 0 

a ~ co ....... I ....... 

O'l P REV FRAMe ROLL CRA8 STEREO +/- FEET SI G X SIG Y ME PITCH ROLL IN-TRACK X-TRACK IN-TRACK X-TRACK IN-TRACK X-TRACK CD Z C11 0 tJj 0 21 5 -1.41 2.5 2F 1800. .510 -.176 .398 .311 .523 -.180 1.069 -.201 .54&- -.021- "" «: (') 

::l (1) 0 21 6 -1.41 2.5 2A 1800. 1.06B .390 .823 .656 1.094 _'tOO 1.599 .379 .505- -.021+ 0 tr! ..... 0 21 5- 6 ST EREO PAIR 1800. .829 .147 .675 .505 .096 .849 .151 1.372 .130 .523- - .. 021 + M «: :3 0 21 1 -33.32 2.0 2v 1800. .252 -1.003 .737 .154 -.486 .240 -1.031 .765 -1.092 .525- -.061- M t>:! 

"" ~ p 0 21 8 -29.77 2.5 2A 1800. .742 -.311 .579 .477 .. 756 -.330 1.251 -.386 .495- -.056- CD ::l 0 21 -41.12 1.5 2F 1900. .687 -.627 .670 .341 .689 -.658 1.242 -.738 .553- -.080- C)1 

t:"" 0 22 9 11.72 2.5 IF 1100. .654 -.772 .718 .. 448 .679 -.781 1.395 -.762 .716- .019+ 

0 

0 

22 

22 

10 

9-10 17.7 

S 

2 

TER EO 

2.5 

PAIR 

IA 1100. 

1100. 

1.413 

1.033 

-.707 

-.740 

10119 

.940 

.831 

.623 -.437 

1.456 

1.068 

-.107 

-.744 

2.153 

1.774 

-

-.725 

.688 .697-

.706-

*019+ 

.019+ ~ >oj 0 22 18 35.45 2.5 2V 800. .036 -.509 .362 .028 -.207 .042 -.524 .736 -.524 .694- .. 000+ 0 0 22 19 12.76 3.0 2A 900. .385 -.636 .530 .217 .. 396 -.652 1.081 -.646 .685- .. 006+ 0 22 20 -20.56 3.0 2Y 800. - .. 403 -.809 .641 -.275 - .. 489 -.416 -.831 .287 -.817 ~7D3+ .014+ Z 0 22 21 20.56 3.0 2A 1640. ,. 276 -1.067 .784 .104 .288 -1.094 .988 -1.093 .700- .001+ 0 22 23 43.24 2.0 2Y 1000. .642 -1.468 1.139 .437 -.449 .672 -1.509 1.373 -1.521 .701- -.012- >oj 

D 23 11 31.19 2.5 2Y 1450. -.005 -.958 .686 t>:! .003 -.434 .003 -.987 1.071 -.985 1.068- .002+ > 0 24 9 -38.99 1.5 2F IlOO. -.273 -1.552 1.116 -.342 -.318 -1.579 1.218 -1.567 1.536- .012+ ~ 0 24 10 -39.70 2.0 2A !lOa. -.,216 -.807 .. 596 -.066 -.240 -.821 1.278 - .808 1.518- .013+ 0 24 9-10 STEREO PAIR lIDO. -.249 -1.233 .930 -.129 -.499 -.284 -1.255 1.244 -1.242 1.528- .013+ 0 24 12 -9.21 2.5 IF 1100. .944 -.582 .787 .570 .966 -.599 2.486 -.584 1.520- e 015+ 0 24 13 -9.21 2.5 IA 1100. .996 -.054 .709 .619 1.021 -.059 2.518 -.044 1.497- .015+ 0 24 12-13 STEREO PAIR IlOO. .970 -.318 .749 .603 -.208 .993 -.329 2.502 -.314 1.509- .015+ a 24 14 32.61 2.5 2F 1700. .374 -.842 .654 .318 .397 -.857 1.916 -.843 1.519- .014+ 0 24 15 33.32 2.0 2A 1600. .852 -1.236 1.070 .424 .893 -1.253 2.409 -1.239 1.516- .. 014+ 0 24 14-15 STEREO PAl R 1642. .653 -1.072 .920 .386 -.466 .687 -1.088 2.203 -1.074 1.516- .. 014+ D 24 16 32.61 2.0 2V 1350. .096 -.519 .317 .069 -.231 .106 -.531 1.626 - .518 1.520- .013+ 0 24 17 -40.41 2.0 2v 1400. -1.620 -.215 10157 -1.090 -.084 -1.663 -.lY6 -.152 - .. 181 1.511+ .. 015+ 

D 25 12 12.76 2.0 2F 900. .255 -.420 .351 .174 .266 -.426 .548 -.386 .282- .. 040+ a 25 15 -33.32 1.5 2F 1000. -.316 -.447 0393 -.238 -.332 -.452 -.028 - .. 427 .304+ .025+ 

§; 0 25 16 -33.32 1.5 2A 1000. d63 -.269 .228 .120 .162 -.278 .442 -.253 .280- .. 025+ 0 25 15-16 SHRW PAIR 1000. -.031 -.343 .308 -.014 -.142 -.044 -.350 .246 -.326 .290- .024+ §; D 25 19 -40.41 2.5 2A 980. .053 -.573 .410 .086 .044 -.589 .321 -.562 .277- .027+ 

~ 0 25 20 7.09 2.5 2V 1400. -.090 -.699 .512 -.058 -.454 -.089 -.118 .200 -.665 .289- .. 053+ 0 25 21 1.41 3.0 IF 980. -.360 -.857 .658 -.214 -.367 -.881 -.OB6 -.829 .281+ .. 052+ to ~ 0 25 22 1.41 3.0 lA 980. -.056 -.763 .542 -.047 -.055 -.783 .214 -.730 .269- .053+ 

H 0 25 21-22 STEREO PAl R 980. -.208 -.810 .602 -.133 -.546 -.211 -.832 .064 -.780 .275+ .052+ to 1-3 0 26 6 -16.30 1.0 2V BOO. -.272 -.186 .248 -.170 -.104 -.282 -.184 .146 -.173 .428+ .011+ 1-1 a 26 1 32.61 1.5 IF 600. .227 -.600 .460 .200 .259 -.596 .688 -.563 .429- ..033+ 1-3 0 26 8 32.61 1.5 lA 600. .681 -.250 .518 .381 .709 -.224 1.132 -.189 .423- .035+ 0 26 7- STEREO PAIR 600. .454 -.425 .490 .228 -.170 .484 -.4!l .910 -.377 .426- .. 034+ D 26 9 5.67 1.5 2V 600. -.342 -.758 .594 - .. 213 -.473 -.346 -.772 .078 -.746 .. 424+ .026+ 0 26 10 -1.41 2.0 IF 600. -.177 -.550 .412 -.104 -.182 -.558 .250 -.534 .432- ..024+ 0 26 II -1.41 2.0 IA 600. .324 -.532 .444 .192 .333 -.542 .759 -.516 .426- .026+ 0 26 10-11 STEREO PAl R 600. .074 -.541 .428 .043 -.344 .076 -.550 .504 -.525 .428- .025+ 0 26 12 -35.45 1.0 2F 960. -.311 -.989 .736 -.293 -.350 -.996 .071 -.984 .421+ .012+ D 26 13 -35.45 1.0 2' 960. .132 -.768 .554 .135 .1l3 -.788 .530 -.776 .417- ,.012+ 0 26 12-13 SHRED PAl R 960. -.089 -.819 .651 - .. 055 -.349 -.118 -.892 .301 -.880 .419- .012+ 0 26 14 -41.B3 1.5 2A 680. .158 -.671 .489 .150 .138 -.691 .548 -.681 .410- ...010+ 0 26 15 -38.99 1.5 2V 1I00. -.001 -.649 .467 -.013 -.259 -.021 -.661 .391 -.648 .412- .. 013+ 0 26 16 ::r:: -4.25 2.0 2F 700. .310 -.387 .355 .185 .317 -.395 .740 -.362 .423- .033+ 0 26 17 P -4.25 2.0 2A 700. .472 -.076 .343 .288 .483 -.078 .888 -.045 .405- ..033+ 0 26 16-17 STEREO PAIR 700. .383 -.245 .350 .233 -.159 .392 -.251 .B07 -.218 .415- .. 033+ () ::l 0 26 18 5.67 2.5 2F 700. -.387 -.580 .495 -.222 -.394 -.594 .018 -.555 .412+ .039+ 0 0- 21.27 2.5 2F 700. -.242 -.514 .405 -.109 -.241 -.529 .183 -.482 .. 424+ .047+ a 0 26 19 ....... 

(1) 0 26 20 21.27 2.5 2A 700. .134 -.086 0120 .077 .139 -.OB6 .527 -.039 .388- .047+ 0 26 19-20 STEREO PAIR 700. -.054 -.300 .298 -.046 -.173 -.051 -.308 .355 -.260 .406- ..048+ ""i <: 0 26 21 26.23 2.0 2A 700. .357 -.215 .318 .205 .369 -.214 .164 - .163 .395- ..051+ 0 ..... 0 26 22 41.12 1.5 2V 900. .488 -.679 .594 .332 -.230 .518 -.682 .931 ..... p -.619 .413- ..063+ 0 26 23 26.94 2.0 2A 700. 1 O'l .. 041 -.566 .845 .6!l 1.082 -.565 1.478 -.510 .396- ..055+ 0 26 24 23.39 2.0 2' 960. 1.054 -.560 .. 844 .620 1.0B7 tJj -.560 1.497 -.506 • .410- ..054+ 0 26 25 13.47 2.5 2v 1200. .414 -.849 .697 0 .281 -.523 .430 -.868 .852 -.816 .422- .052+ ::l «: 0 26 26 18.43 2.5 2A 1100. .812 -,373 .635 .487 .836 -.375 1.242 -.320 .406- .055+ ....... (1) 

0 26 27 24.10 2.0 2A 1160. .505 -.339 .441 .293 .521 -.342 .919 -.283 .398- .059+ «: 0 26 28 27.65 2.0 2A 1033. .648 -.445 .564 .373 :3 .670 - .. 44l 1.061 -.386 .391- .0&1+ 

~ P 

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Approved for Release: 2018/09/11 COS10302S 
- -

:> , 

01>-

-

PHOTU 

I .D. 

ReV FRAME 

o 27 

o 27 4 

D 27 3- 4 D 27 10 

D 27 11 

o 27 ID-11 

D 27 12 

D n 13 

D 27 12-[3 

D 27 14 

o 27 15 

o 27 14-15 

D 31 1 

o 31 2 

D 31 3 

o 31 2- 3 

o 31 4 

D 31 5 

31 4- 5 

31 6 

D 32 

D 32 

o 32 

D 32 

D 32 

D 32 

D 32 

o 34 

D 34 

D 34 

o 37 

o 37 

D 37 

o 37 

D 37 

D 37 

D 37 

o 37 

D 38 

o 38 

o 38 

o 38 

o 38 

o 38 

D 38 

o 38 

D 38 

D 39 

o 39 

40 

o 4D 

o 4D 

o 40 

o 40 

o 40 

D 40 

D 40 

o 40 

o 40 

o 40 

4 

5 

4-

6 

7 

2 

3 

2-

5 

6 

7 

B 

7- B 

9 

10 

9-10 

13 

14 

13-14 

15 

21 

27 

28 

27-28 

29 

13 

14 

4 

3- 4 

7 

12 

13 

12-13 

14 

15 

14-15 

17 

-

ROll 

-

COMI<ANOEO 

POSITIDN 

CRAB STERED 

33.32 1.5 IF 

33.32 1.5 II STEREO PAIR -24.81 2.D IF 

-24.81 2.0 11 

STEREO PAIR 

26.23 2.5 IF 

26.23 2.5 lA 

STEREO PAIR 

-37.57 2.5 IF 

-37.57 2.5 11 

STEREO PAIR 

-26.94 2.5 2V 

-15.59 2.5 IF 

-15.59 2.5 lA 

STEREO PAIR 

-2.83 3.0 2F 

-2.83 3 .. 0 2A 

STEREO PAIR 

-2.12 3.0 2V 

-.70 2.5 2V 

-2.12 2.5 2V 

-20.56 2.5 IF 

-20.56 2.5 1A 

STEREO PAIR 

-4.96 3.D 2V 

19.85 2.5 21 

2.12 3.5 2F 

2.12 3.5 2A 

STEREO PAIR 

-39.70 L,5 2V 

4.25 2.0 2V 

-29.06 2.0 2F 

-29.06 2.0 2A 

STEREO PAl R 34 .. 03 2.0 2F 

34.03 2.0 21 

STEREO PAIR 

-24.10 2.5 2F 

-24.10 2.5 21 

STEREO PAIR 

-44.66 2.0 2V 

-ll.34 3.0 2V 

-38.28 3.0 2F 

-38.99 3.5 2A 

STEREO PIIR 

-31.9D 3.5 2A 

-38.99 2.5 2V 

-44.66 2.0 2V 

36.15 1.5 2F 

36.86 1.0 2A 

STEREO PAIR 

-19.14 2.0 2V 

17.72 2.5 IF 17.72 2.5 lA 

STEREO PAIR 

-26 .. 94 2 .. 0 2F 

-26.94 2.5 2A 

STEREO PA!R 

26.94 2.5 2V 

MAP 

ACCURACY 

+/- FEET 

10DD. 

1000. 

1000. 

88D. 

880. 

880. 

15 DO. 

1500 .. 

15 DO. 

2000. 

2000. 

2000. 

700. 

70D. 

700. 

700. 

40D. 

40D. 

40D. 

40D. 

400. 

400. 

400. 

40D. 

400. 

400. 

400. 

150D. 

150D. 

15DD. 

168D. 

1500. 

1600. 

160D. 

160D. 

1400. 

1400. 

1400. 

1740. 

1600. 

1654 .. 

700. 

1460. 

170D. 

1700. 

1700. 

18DO. 

1600. 

1400. 

1600. 

1600. 

160D. 

90D. 

2DOD. 

2000. 

2000. 

1025. 

80D. 

929. 

1375. 

GEO-POSITIONI~lG 

IHSS DISTANCE 

NAUTICAL MILES 

51 G x 

-.748 

.369 

-.19D 

-.540 

- ... 248 

-.394 

-.977 

-.257 

-.617 

-.605 

-.464 

-.535 

.214 

.158 

.684 

.433 

.329 

.709 

.519 

-.160 

-.033 

-.179 

-.754 

-.207 

-.480 

.291 

.915 

-.498 

-.068 

-.283 

-.354 

.557 

.375 

.872 

.623 

.787 

1.529 

1.158 

.228 

.583 

.. 446 

-.266 

.045 

.297 

.754 

.526 

1.144 

.652 

.120 

.603 

1.525 

1.141 

.297 

.756 

1.07D 

.913 

-.313 

.D49 

-.158 

1.0D2 

S I G Y 

-[.031 

-1.088 

-1.D59 

-.268 

-.081 

-.174 

-.534 

-.398 

-.466 

-1.477 

-1.526 

-1.5Dl 

-1. ll5 

-.301 

-.337 

-.320 

-.[76 

-.277 

-.227 

-.499 

-.284 

-.954 

-1.005 

-I.! 75 

-1.090 

-.266 

-.405 

-.725 

-.619 

-.672 

-1.050 

-.439 

-.958 

-.261 

-.609 

-.370 

.046 

-.162 

-1.177 

-1.349 

-1.283 

-1.367 

-.635 

-1.023 

- .. 560 

-.792 

-.305 

-.482 

-1..122 

-.360 

-1.380 

-.955 

-1. 443 

-.800 

-.330 

-.565 

-.969 

-.333 

-.696 

-.883 

ME 

.904 

.813 

.860 

.430 

.[94 

.334 

.788 

.338 

.606 

1.136 

1.137 

1.137 

.815 

.. 248 

.545 

..429 

.269 

.539 

.426 

.4DO 

.247 

.688 

.891 

.847 

.869 

.286 

.710 

.622 

.441 

.539 

.788 

.503 

.731 

.647 

.69D 

.618 

1.084 

.882 

.853 

1.042 

.974 

.989 

.466 

.755 

.665 

.712 

.839 

.583 

.805 

.505 

1.457 

1.160 

1.044 

.788 

.801 

.795 

.732 

.241 

.576 

.968 

ATTITUDE ERRORS 

DEGREES 

PITCH 

-.298 

0145 

-.071 

-.350 

-.149 

-.232 

-.571 

- .194 

-.380 

-.542 

-.154 

-.332 

.175 

• D86 

..441 

.267 

.2 D6 

.448 

.326 

-.109 

-.023 

-.122 

-.543 

-.075 

-.316 

.198 

.. 557 

-.304 

-.053 

-.180 

-.250 

.370 

.148 

.558 

.393 

.525 

.956 

.633 

.065 

.443 

.280 

-.195 

.030 

.077 

.476 

.299 

.668 

.450 

.073 

.388 

.802 

.667 

.183 

.526 

.659 

.553 

-.273 

.052 

- .086 

.683 

ROLL 

- .. 446 

-.087 

-.267 

-.637 

-.613 

-.193 

- .. 153 -.338 

-.191 

-.649 

-.648 

-.181 

-.454 

- .. 409 

-.286 

-.303 

-.080 

-.742 

-.477 

-.422 

-.297 

-.220 

-.401 

-.336 

-.855 

-.335 

-.375 

-.446 

- - - OAT A 

EPHEI~ER I S ERRORS 

NAUTICAL MILES 

REST FIT COMi'>1A~D COMMAND - SF E 

IN-TRACK X-TRACK IN-TRACK X-TRACK IN-TRACK X-TRACK 

-.714 

.432 

-.141 

-.557 

-.255 

-.406 

- .996 

-.259 

-.628 

-.636 

-.491 

-.564 

.268 

.161 

.700 

.442 

.337 

.726 

.. 532 

-.164 

-.033 

-.183 

-.778 

-.219 

-.4'98 

.298 

.. 940 

-.510 

-.069 

-.289 

-.392 

.572 

.369 

.890 

.630 

.813 

1.566 

1.190 

.224 

.586 

.447 

-.297 

.045 

.308 

.777 

.542 

1.177 

.662 

.108 

.639 

1.645 

1 .. 226 

.286 

.781 

1.100 

.940 

-.331 

• D47 

-.169 

I.D33 

-1.076 

-1.083 

-1.080 

-.267 

-.080 

-.174 

-.559 

- .. 411 

-.485 

-1.516 

-1.560 

-1.538 

-1.147 

-.310 

~ .. 349 

-.330 

-.181 

-.284 

-.233 

-.513 

-.291 

-.979 

-1.029 

-[.204 

-1.117 

-.273 

- .. 410 

-.749 

-.635 

-.692 

-1.062 

-.447 

-.985 

-.280 

-.633 

-.364 

.D78 

-.143 

-1.211 

-1.388 

-1.320 

-1.399 

-.654 

-1.055 

-.565 

-.805 

-.306 

-.503 

-1.155 

-.327 

-1.303 

-.894 

-1.475 

-.814 

-.329 

-.571 

-.991 

- .. 342 

-.713 

-.902 

-.[ 34 

.982 

.424 

-.004 

.280 

.138 

-.459 

.261 

-.099 

- .. 114 

.037 

-.D39 

1.482 

[.406 

1.868 

1.647 

1.559 

1.905 

1.732 

1.014 

1.928 

1.746 

1.163 

1.669 

1.416 

2.205 

2 .. 833 

.221 

.667 

.444 

.291 

1.257 

1.036 

1.565 

1.301 

1.503 

2.225 

1.864 

.. 489 

.832 

.700 

-.037 

.291 

.544 

1.022 

.783 

1.419 

.976 

.418 

1.064 

2.041 

1.634 

.674 

1.177 

1.479 

1.328 

.072 

.415 

.219 

1.408 

-1.048 

-1.054 

-1.051 

-.237 

-.050 

-.144 

-.492 

-.344 

-.418 

-1.473 

-1.517 

-1.495 

-1.197 

-.336 

-.372 

- .355 

-.181 

-.284 

-.232 

-.506 

-.291 

-.979 

-1.059 

-1.231 

-1.145 

-.270 

-.367 

-.778 

-.664 

-.721 

-1.117 

-.475 

-1.035 

-.329 

-.682 

-.373 

.070 

-.151 

-1.250 

-1.427 

-1.359 

-1.448 

-.688 

-1.078 

-.587 

-.828 

-.329 

- .. 546 

-1.20[ 

-.326 

-1.301 

-.893 

-1.510 

-.837 

-.352 

-.594 

-1.032 

-.382 

-.753 

-.926 

.580+ 

.55 D-

.565-

.. 553+ 

.535-

.. 544+ 

.537+ 

.520-

.52'9+ 

.522+ 

.528+ 

.525+ 

1.214-

1.245-

1.16 B1.2D5-

1.222-

1.179-

1.200-

1.1 78-

1.961-

1.929-

1.941-

1.888-

1.914-

1.907-

1.8'93-

.731+ 

.736-

.733-

.683+ 

.685-

.667-

.675-

.671-

.690-

.659-

.674-

.265-

.246-

.253-

.260+ 

.246-

.236-

.245-

.241-

.242-

.314-

.310-

.. 425-

.396-

.4D8-

.388-

.396-

.379-

.388-

.403+ 

.368-

.388-

.375-

.D28+ 

.029+ 

.. 029+ 

'" 03D+ 

..030+ 

.030+ 

.067+ 

.067+ 

.. 067+ 

.. 043+ 

.043+ 

.. 043+ 

-.050-

-.026-

-.023-

-.025-

.000+ 

.. 000+ 

.001+ 

.007+ 

.000+ 

.. 000+ 

-.030-

-.027-

-.D28-

.003+ 

.043+ 

-.029-

-.029~ 

-.029-

-.055-

-.028-

-.050-

-.049-

-.049-

-.009-

-.008+ 

-.008-

-. D39-

-.039-

-.039-

-.049-

-.034-

-.023-

-.022-

-.023-

-. D23-

-.043-

-.046-

.. 001+ 

.. 002+ 

.001+ 

-.035-

-.023-

-.023-

-.023-

- .. 041-

-.040-

-.040-

-.024-

- - -

Approved for Release: 2018/09/11 C05103025 __________________ _ 
- - - - - - - - - - C05'103025-

- - - - - - Approved for Release: 2018/09/11 

::r: G E 0 - p 0 S I T I 0 N I N G 0 A T A 

pJ ::0 "0 ttl 

() ;:I t':I tr! () PHOTO COMMANDED f.1AP MIS.'::. OISTAI<CE A TT !TUDE ERRORS E: PHE:>lER I S ERRORS "0 ::0 CIl 0 0.. 

0 '-rJ C..:> ....... a ('I) 1.0. PDSITION ACCURACY NAUT I CAL MILES DEGREES r,AUT ICAL MIUS ::0 @ w '"i >-1 -J 

0 ..... 

<: BES T FIT CO,\lMANO COMMAND - BFE C..:> 

z ~ ....... w pJ , Ul REV FRAME RO LL CRAB STEREO +/- FEET SIG X SI G Y ME DITCH ROLL IN-TRACK X-TRACK IN-TRACK X-TRAr:K IN-TRACK X-TRACK 0 0"> ttl Z a! 0,< 0 41 24 -12.05 2.5 IF 1000. -.504 -1.265 a 969 -.360 -.521 -1.297 -1.222 -1.319 -.701- -.022- ..,. () ;:I ('I) 0 41 25 -12.05 2.5 lA 1000. -.281 -1.066 .787 -.149 -.292 -1.093 -1.005 -1.114 -.713- -.021- 0 tr! 

~s 0 41 24-2;' STEREO PAIR 1000. - 0382 -1.157 .. 874 -.239 -.751 -.396 -1.185 -1.103 -1.207 -.707- -.022- N 0 41 26 -27.65 2.5 2A 900. -.622 -1.153 .928 - .316 -.649 -1.176 -1.379 -1.205 -.730- -.029- N trl 

pJ 0 41 27 -34. "'4 2.5 2A 1000. -.586 -1.2D2 .949 -.271 -.615 -1.226 -1.333 -1.258 -.718- -.032- "-

;:I ~ () 41 29 -25.52 2.5 2f 1500. .838 -.964 .905 .461 .853 -.999 .151 -1.019 - .. 702+ -.020- 0"> [, 41 3D -25.52 3.0 2A 1500. 1.075 -.373 .805 .705 1.100 -.390 .388 - .409 -.712+ -.019- a! 

0 41 29-30 STEREO PAIR 1500. .957 -.669 t'" .856 .607 -0376 .976 - .693 .269 -.713 -.707+ -.020-

~ 41 31 -21.27 3.0 3F 2000. -.306 -.027 .224 -.195 -.313 -.027 -1.027 -.041 -.714- -.014- 41 32 -24.10 3.0 3A 2000. .016 - .. 395 .286 .033 .015 -.4D6 -.709 -.420 -.724- -.014- 0 41 31-32 STEREO PA I R 2000. -.145 -.211 .257 -.101 -.117 -.149 -.217 -.868 -.232 -.719- -.015- >-1 

..... D 42 5 38.99 1.5 2F 700. 10161 -.953 1.065 .799 1.238 -.904 .337 -.880 - .. 901" .. 024+ 0 [) 42 6 38.99 1.5 2A 725. 1.721 .318 1.239 1.043 1.746 .412 .806 .435 - .940+ .023- Z D 42 5- 6 STEREO PArR 711. 1.410 -.388 1.146 .644 -0131 1.463 -.322 .545 -.299 -.918+ .023+ 0 42 >-1 8 -20.56 1.5 2V 600. -.216 -1.360 .975 -.154 -.774 -.245 -1.378 -1.169 -1.419 -.924- - .. 041- 42 9 -34.03 1.0 IF 600. tr! -.059 -1.343 .952 -.174 -.100 -1.362 -1.002 -1.416 -.902- -.054- 0 42 10 -34 .. 03 1.0 lA 600. .238 -1.174 )- .. 849 .222 .210 -1.203 -.727 -1.256 -.937- -.053-

~ [; 42 9-10 STEREO PAl R 600. .073 -1.268 .907 .015 -.564 .038 -1.292 -.880 -1.345 - .918- -.053- 0 42 11 -9~92 2.0 2F 600. .020 -.665 .473 -.007 .016 -.676 -.884 -.706 - .. 900- -.030- 0 42 12 -9.92 2.0 2A 600. 0319 -.273 .301 .199 .325 -.280 -.619 -.309 -.944- -.029- 0 42 11-12 STEREO PAIR 600. 0169 -.469 .396 0104 -.295 .171 -.479 -.751 -.508 -.922- -.029- o 42 13 -14.88 2.0 2V 700. -.375 -.530 .460 -.248 -.326 -.389 -.536 -1.319 -.569 -.930- -.033- 0 42 14 -41.12 1.5 2V 660. -.559 -.795 .691 -.380 -.293 -.598 -.793 -1.542 -.852 - .944- -.059- 42 15 -35 .. 45 2.0 2A 700. .563 -.237 .437 .363 .571 -.256 -.381 -.307 -.952+ -.051- 0 42 16 -15.59 2.0 2F 600. .586 -.503 .549 .339 .597 -.518 -.326 -.548 -.923+ -.030- D '.2 17 -15.59 2.0 2A 600. .859 .055 .609 .. 530 .881 .050 -.065 .020 -.946+ -.030+ 0 42 16-17 S TfRED PA IR 600. .708 -.255 .576 .440 -.154 .723 -.266 -.210 -.296 - .. 933+ -.030- 0 42 18 -6 .. 38 2.0 2. 600. 1 .. 053 -.368 .795 .655 1.078 -.378 .135 -.401 - .9'+3+ --.023- 0 42 19 -7. 79 2.0 2F 600. .442 -.754 .623 .259 .451 -.772 -.481 -.797 -.932- -.025- 0 42 20 -7.79 2.0 2' 600. .684 -.569 .635 .433 .700 -.584 -.246 -.607 -.946+ -.023- D 42 19-20 STEREO PAIR 600. .563 - .. 661 .629 .348 -.434 .. 575 -.678 -.364 -.702 - .. 939+ -.024-

§; 0 42 21 19.85 2.0 2V 660. .411 -.428 .427 .277 -.244 .426 -.433 -.505 -.439 -.931- -.006- 0 42 22 -8.50 2.5 2F 600. -.188 -.760 .555 -.134 -.195 -.777 -1.143 -.800 - .948- -.023- 0 42 23 -8.50 2.5 2A 600. .286 -.607 .476 .188 .292 -.623 -.665 -.645 -.957- -.022- §; 0 42 22-23 STEREO PAl R 600. .049 -.683 .517 .029 -.449 .048 -.700 -.904 -.723 -.952- -.023-

~ 0 42 24 -19.85 2.5 2V 700. .003 -.749 .547 -.002 -.460 -.003 -.768 -.954 -.796 -.951- -.028-

l-I 

to D 

0 

0 

42 

42 

42 25-26 

26 

2, -26.94 

-26.94 

STEREO 

2. 

2.0 

a 

PAl R 

lA 

IF 1000. 

1000. .563 

.030 

-.418 

-.746 

.498 

.530 -.041 

.380 .572 

.022 -.765 

-.434 -.391 

-.903 -.798 

-.466 

-.925-

- .. 963+ -.032-

-.033- ~ 1000. .296 -.582 .514 .186 -.301 .297 -.600 -.647 -.632 -.944- -.032- to 1-:3 0 42 27 -34.03 2.5 2A 800. .520 -.588 .560 .375 .525 -.611 -.435 -.647 -.960+ -.036- l-I D 42 28 -4.25 3.0 IF 600. 0120 -.697 .502 .071 .123 -.716 -.824 -.733 - .94 7- -.017- 0 42 29 -4.25 3.0 lA 600. .442 -.219 .351 1-:3 .281 .453 -.225 -.509 -.241 -.962- -.016- 0 42 28-29 STEREO PA IR 600. .281 -.458 .433 .178 -.309 .288 -.470 -.666 -.487 -.954- -.017-

0 43 -13.47 1.0 IF 740. -.745 -1.233 1.020 -.487 -.783 -1.234 -1.951 -1.272 -1.168- -.038- 0 43 -13.47 1.0 l' 740. -.214 -.706 .524 -.109 -.231 -.712 -1.419 -.750 -1.188- -.038- 0 43 4- STEREO PAl R 74D. -.480 -.969 .810 -.280 -.563 -.507 -.974 -1.685 -1.012 -1.178- -.038- 0 43 6 -26.94 1.0 2F 900. -.769 -10162 .986 -.549 -.825 -1.151 -2.007 -1.204 -1.182- -.053- 0 43 9 13.47 1.5 IF 1920. -.366 -10132 .843 -.162 -.359 -1.152 -1.526 -1.162 -1.167- -.010- 0 43 10 13.47 1.5 lA 1933. .477 -1.088 .844 .248 .506 -1.098 -.715 -1.108 -1.221- -.010- D 43 9-10 STEREO PAIR 1927. .094 -1.108 .843 .057 -.671 .113 -1.123 -1.083 -1.133 -1.196- -.010- 0 43 13 36.86 2.0 IF 420. .321 -.630 .502 .268 .348 -.630 -.848 -.616 -1.196- .014+ ::r: 43 14 36.86 2.0 lA 420. 1.166 .261 .849 .731 1.186 .303 -.039 .317 -1.225+ .014- 43 13-14 STEREO PA JR 420. .743 -.184 .697 .346 -.086 .767 -.165 -.443 -.151 -1.210+ .014+ pJ 43 17 39.70 2~O 2F 600. .671 -1.497 1.161 .603 .734 -1,.505 -.437 -1.486 -1.171" .019+ () ;:I 43 18 39.70 2.0 2A 600. 2.185 -1.482 1 .. 868 1. 205 2.285 -1.445 1.052 -1.426 -1.233+ .019+ 0 0.. 43 17-18 STEREO PAIR 600. 1.428 -1.490 1.555 .761 -.520 1.510 -1.475 .307 -1.457 -1 .. 203+ .018+ ;:I ....... 43 19 39 .. 70 1.5 2A 700. 1.800 -1.411 1.620 .982 1.884 -1.391 .665 -1.377 -1.219+ .014+ ,...,.. ('I) 

0 43 20 -8.50 2.5 IF 1000. .483 -1.239 .942 .281 .492 -1.271 -.729 -1.292 -1.221- -.021- '"i 0 43 21 -8.50 2.5 lA 1000. <: .797 -.586 .701 .509 .815 -.602 -.418 -.623 -1.233+ -.021- 0 ..... 0 43 2D-21 STEREO PAI R 1000. .. 640 -.912 .830 .404 -.607 .654 -.937 -.574 -.958 -1.22B+ -.021- ....... pJ Ul 0 47 7 -.70 2.5 2V 927. .022 -.646 .491 .0 15 -.437 .023 -.663 .255 - .686 .232- -.023- ° ttl 0 47 8 -20.56 j.O 2A 900. .054 -.658 .470 .066 .052 -.676 .294 -.689 .242- -.013- D 47 9 -5.67 3.0 2V 900. -.321 -.360 ;:I '< .347 -.219 -.245 -.329 -.370 -.088 -.391 .. 241+ -.021- 0 47 ...... ('1) 10 -22.68 j.O 2F 900. -.394 -.925 .715 -.308 -.409 -.951 -.180 -.962 .229+ -.011- '< S 47 11 -; 2 .68 3.0 2A 900. .. 0:-'3 -.703 .503 .070 .050 -.722 .302 -.733 .252- -.011- 47 10-1, STERdJ PA I K 90U. -.171 -.814 .618 - 0106 -.474 -.179 -.836 .061 -.847 .240+ -.011- pJ > , ;:I 

a! 

____ Approved for Release: 2018/09/11 C05103025 
-

:x:-

I 

0') 

- -

PHOTO 

I .. U. 

REV FRt\l'>'\E 

U 48 6 

D 48 7 

48 6- 7 

iJ 48 8 

48 9 

48 8- Y 

[) 48 10 

D 48 11 

[j 48 12 

o 53 

D 53 9 

D 53 8- <} 

D ;4 

o 5.ft 

D 54 

D 54 

o 54 

D 54 

D 54 

D 54 

D 54 

o 54 

o 54 

D 54 

o 54 

o 54 

o 54 

D 54 

o 54 

54 

o 55 

o 55 

D 55 

o 55 

D 55 

o 55 

D 55 

o 55 

D 55 

o 56 

D 56 

D 56 

o ;6 

D 56 

o 56 

o 56 

D 56 

o 57 

o 57 

o 57 

o 58 

o 58 

D 58 

o ;8 

D 58 

o 58 

D 58 

II 

12 

11-12 

13 

14 

15 

14-15 

16 

20 

21 

20-21 

22 

23 

24 

23-24 

39 

40 

39-40 

17 

18 

17-18 

19 

20 

19-20 

21 

22 

21-22 

9 

10 

9-10 

12 

13 

12-13 

24 

25 

21 

22 

21-22 

4 

5 

4-

6 

9 

10 

9-10 

- - - A~ved furRele~ 2018'i0'9/11 'Co510302S1 

- - - - - - COMMANDED 

PUSITION 

ROLL CRAB 

7.79 2.5 

7.79 2 .. 5 

STEREO PAIR 

-1.41 2.5 

-1.41 2.5 

SH:REO PAIR 

1.41 255 

3.54 2.5 

.. 70 3 .. 0 

-29.06 3 .. 0 

-29.06 3.0 

STEREO PAIR 

SHRED 

2F 

2A 

IF 

IA 

2A 

2V 

2V 

IF 

lA 

24.10 2.0 IF 

24.10 2.0 lA 

5TEREO PAIR 

4.25 2.5 2V 

-19.85 2 .. 5 2F 

-19.85 2.5 2A 

STEREO PAIR 

20.56 2.0 2V 

-3.54 3.0 IF 

-3.54 3.0 lA 

STEREO PAIR 

-.70 2.5 2V 

-26.23 2.5 2F 

-26.23 2.5 2A 

STEREO PAIR 

-34.03 3.0 2F 

-34.03 3eD 2A 

STEREO PAIR 

17.01 3.0 IF 

17.01 3.0 lA 

STEREO PAIR 

-8.50 3.5 IF 

-8.50 3.5 lA 

STEREO PAIR 

24.81 3.0 2F 

24.81 3.0 2A 

STEREO PAIR 

23.39 2.0 

23.39 2.0 

STEREO PAIR 

-27.65 2.0 

-27.65 2 .. 0 

STEREO PAIR 

-42 .. 54 2.5 

-41.83 2.5 

2F 

2A 

2F 

2A 

2V 

2V 

-31.19 3.0 IF 

-31.19 3.0 lA 

STEREO PAIR 

-1.41 1.5 IF 

-1.41 1.5 IA 

STEREO PAIR 

.00 1.5 2V 

9.92 2.0 IF 

9.92 2.0 lA 

STEREO PAIR 

MAP 

ACCliKACY 

+/- FEET 

1000. 

1000. 

1000. 

1000. 

1000. 

1000. 

1000 .. 

10008 

1000. 

1600. 

1600. 

1600. 

1200. 

1200. 

1200. 

1020. 

1200. 

1200. 

1200. 

1300. 

15DO. 

1467. 

1482. 

900. 

880. 

880. 

880. 

1900. 

1900. 

1900. 

1467. 

1520. 

1491. 

1300. 

1300. 

1300. 

957. 

940 .. 

950. 

700. 

700. 

700. 

1333. 

1340. 

1336. 

1200. 

1300. 

1100. 

1100. 

1100. 

900. 

900 .. 

900. 

1900. 

8 DO. 

800. 

800. 

G E 0 - P 0 SIT ION I !~ G 

MISS UI:,TIHKE 

T~AUT I CAL i-t I LI::,S 

S I G X 

.208 

.658 

.433 

.094 

.256 

.175 

-.!l 7 

-.643 

-.143 

.524 

.628 

.576 

- .. 031 

.888 

.. 470 

.603 

.359 

.678 

.50 I 

.. 908 

-.159 

.208 

.041 

-.335 

-.528 

-.297 

-.413 

-.423 

-.227 

-.325 

-.455 

-.104 

-.296 

.258 

.665 

.462 

-.475 

-.030 

-.290 

.832 

1.597 

1.215 

-.171 

-.013 

- .. 099 

.246 

.458 

.470 

.935 

.703 

.387 

.852 

.619 

.315 

.224 

.874 

.564 

SI G Y 

-1.104 

-.646 

-.875 

-1 .. 032 

-.637 

-.83' 

-~315 

-.568 

-.434 

-1.313 

-.865 

-1.089 

-.763 

-.391 

-.560 

-.440 

-1.249 

-.849 

-1.072 

.087 

-.690 

-.663 

-.675 

-.702 

-1.121 

-1.305 

-1.213 

-1.306 

-1.227 

-1.266 

-.627 

-.035 

-.358 

-.135 

-.669 

-.702 

-.663 

-.771 

-.708 

-1.287 

-1.362 

-1.324 

-1.977 

-2.139 

-2.050 

-1.246 

-.933 

-.729 

-.400 

-.565 

-.303 

-.016 

-.160 

-.257 

- .. 461 

-.513 

-.488 

I.jE 

.795 

.654 

.728 

.733 

.488 

.623 

.248 

.608 

.328 

1.002 

.762 

.890 

.. 548 

.689 

.629 

.. 529 

.923 

.774 

.860 

.645 

.506 

.498 

.501 

.556 

.878 

.947 

.913 

.914 

.886 

.931 

.. 557 

.114 

.418 

.552 

.668 

.613 

.582 

.551 

.569 

1.085 

1.485 

1.301 

1.407 

1.516 

1.458 

.904 

.740 

.619 

.723 

.673 

.355 

.606 

..496 

.306 

.366 

• 7I 9 

.578 

ATT fTU~)::: ERROl(.S 

UEGREES 

PITCH 

.170 

.397 

.266 

.061 

.162 

.110 

-.077 

- .. 440 

- .098 

.216 

.422 

.. 341 

.042 

.532 

.270 

.407 

.158 

.464 

.309 

.614 

-.102 

.131 

.025 

-.228 

-.417 

-.113 

-.273 

-.338 

-.037 

-.175 

-.248 

-.068 

-.199 

.152 

.428 

.291 

-.239 

-.078 

- .157 

.620 

.905 

.741 

-.272 

.126 

-.103 

.155 

.302 

.234 

.618 

.435 

.233 

.518 

.375 

.206 

.156 

.526 

.348 

ROLL 

-.573 

-.571 

-.385 

-.296 

-.541 

-.323 

-.293 

-.653 

.056 

-.459 

-.479 

-.685 

-.557 

-.219 

-.467 

-.367 

-.705 

-1.OB7 

-.472 

-.375 

- .281 

-.103 

-.167 

-.315 

f:PHEr'H::~IS ERRURS 

'~AUTICAL i~ILF.'i 

BEST FIT COMMAN!) - BFf: 

IN-TRACK X-TRACK IN-TRACK X-TRACK ll\i-TRACK X-fRACK 

.218 

.678 

.'+48 

.097 

.263 

.180 

-.120 

-.658 

-.146 

.538 

.. 646 

.592 

-.021 

.915 

.489 

.619 

.358 

.688 

.505 

.929 

-.163 

.213 

.042 

-.343 

-.550 

- .. 314 

-.432 

-.432 

-.231 

-.332 

-.464 

-.106 

-.301 

.264 

.681 

.473 

- .. 484 

-.027 

-.294 

.817 

1.661 

1.269 

-.205 

-.045 

- .133 

.235 

.457 

.477 

.956 

.717 

.397 

.873 

.635 

.324 

.233 

.. 899 

.582 

-I.DO 

-.659 

-.894 

-1.059 

-.653 

- .. 856 

- .323 

-.584 

- .. 446 

-1.356 

-.879 

-1.1l4 

-.780 

-.387 

-.566 

-.449 

-1.282 

-.875 

-1.101 

.098 

-.708 

-.681 

-.693 

-.722 

-1.149 

-1...337 

-1.243 

-1.349 

-1.242 

-1 .. 294 

- .650 

-.036 

-.369 

-.760 

-.687 

-.723 

-.689 

-.791 

-.732 

-1.294 

-1.361 

-1.328 

-2.016 

-2.187 

-2.094 

-1.284 

- .965 

-.756 

- .. 416 

-.585 

- .. 307 

-.017 

-.163 

-.260 

-.468 

-.516 

-.493 

.482 

.954 

.7l8 

.353 

.533 

.. 443 

.156 

-.384 

.125 

.218 

.368 

.293 

-.076 

.850 

.. 429 

.550 

.299 

.627 

.445 

.863 

-.213 

.160 

-.009 

-.395 

-.617 

- .. 367 

-.492 

-.466 

-.229 

-.348 

-.552 

-.184 

-.384 

.175 

.616 

.396 

-.572 

-.095 

- .. 373 

.. 540 

1.258 

.899 

-.559 

-.458 

-.513 

-.209 

.008 

-.153 

.268 

.058 

-.070 

.348 

.139 

-.177 

-.272 

.344 

.051 

-} .! 58 

-.688 

-.923 

-1.083 

- .677 

-. BBO 

-.348 

-.610 

-.470 

-1.315 

-.838 

-1.073 

-.777 

-.385 

-.564 

-.447 

-1.278 

-.871 

-1 .. 098 

.098 

-.707 

-.679 

-.692 

-.721 

-1.142 

-1.331 

-1.237 

-1.331 

-1.226 

-1.278 

-.658 

-.045 

-.378 

-.760 

-.687 

-.723 

-.706 

-.809 

-.749 

-1.267 

-1.333 

-1.300 

-2.093 

-2.263 

-2.j 71 

-1.391 

-1.065 

-.825 

-.481 

-.652 

-.347 

- .. 056 

-.202 

-.295 

-.480 

-.528 

-.505 

.264-

.276-

.270-

.256-

.270-

.263-

.276-

.. 274+ 

.. 271 + 

-.320+ 

-.278+ 

- .. 2 99 + 

-.055-

- .. 065+ 

-.060+ 

-.069+ 

-.059+ 

-.061+ 

- .. 060+ 

-.066+ 

-.050-

-.053+ 

-.051+ 

-.052-

-.067-

-.053-

- .060-

-.034-

.002+ 

-.016-

-.088-

-.078-

-.083-

-.089+ 

- .. 065 + 

-.077+ 

-.088-

-.068-

-.079-

-.337+ 

-.403+ 

-.370+ 

-.354-

- .413-

-.380-

-.444+ 

-.449+ 

-.630+ 

-.688+ 

- .. 659+ 

-.467+ 

-.525+ 

-.496+ 

-.501+ 

-.505-

-.555+ 

-.531+ 

-.028-

-.029-

-.029-

-.024-

-.024-

-.024-

-.025-

-.026-

-.024-

.041+ 

.041+ 

~ 041+ 

.003+ 

.. 002+ 

.002+ 

.. 002+ 

.004+ 

.. 004+ 

.. 003+ 

.000+ 

.001+ 

.002+ 

.001+ 

.. 001+ 

.. 007+ 

.. 006+ 

.006+ 

.. 018+ 

.016+ 

.. 016+ 

-.008-

-.009-

-.009-

.000+ 

.000+ 

.. 000+ 

-.017-

-.018-

-.017-

.. 027+ 

.. 028+ 

.028+ 

-.077-

-.076-

-.077-

-.107-

-.100-

-.069-

-.065-

-.067-

-.040-

-.039-

-.039-

- .. 035-

-.012-

-.012-

- .. 012-

Approved for Release: 2018/09/11 COS10302S __________________ _ 
- - - - - - - - - -- Co5103025' 

- - - - - - Approved for Release: 2018/09/11 

::r: :xl 'ij ttl ~ trl trl l.l (j ::l 'ij :xl til 

0 Q.. 0 >%j t.l a I-' :xl 0 to l'P 

I-j :xl """ .., t.l 

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Ul 0 (j) Z <:.11 

0 ttl >1>- l.l '-< ::l 0 trl l'P ....... t>.:I S G E 0 - P 0 S I T I 0 N I N G 0 A T A t>.:I trl '< ~ "- <: (j) ;..- ::l PHOTO c..UMMANLJEO MAP 1-'11 55 01 S T ANeE ATTITUOE ERRORS EPHEMERIS ERRORS <:.11 

t-< I.Os POSITION ACCURACY NAUTICAL MILES OEGREES NAUTICAL MILES 

~ BE ST FIT COMMANO COMMAND - BFE :j REV FRAME ROLL CRAB STEREO +/- FE ET S I G x SIG y ME PITCH ROLL IN-TRACK X-TRACK IN-TRACK X-TRACK IN-TRACK X-TRACK 0 

Z D 58 Il -10.63 2.0 IF 600. .315 -.735 .567 .173 .319 -.751 -.193 -.801 - .. 512+ -. 05 0- I-j 0 58 12 -10.63 2.0 lA 600. .671 -.937 .816 .437 .683 -.960 .114 -1. 008 - .. 569+ -.048- D 58 11-12 5 TER EO PA trl IR 600. .493 -.836 .702 .299 - .. 539 .501 -.855 - .. 039 - .. 904 -.540+ -.049- 0 58 13 -7.09 2.0 IF 700. ;..- .419 - .. 420 .421 .254 .'t29 - .. 430 - .. 084 -.472 - .. 513+ -.042-

0 

D 

58 

58 

13-14 

1'. -7 .. 09 2.0 lA 700. .918 -.022 .650 .576 .. 940 - .. 025 .368 - .. 065 - .. 572+ - .. 040- ~ STEREO PAIR 700. .669 -.221 .. 548 .420 -.143 .. 685 -.228 .142 -.269 - .. 543+ - .. 041- a 58 15 -11.34 2.5 If 700. .553 -.867 .734 .322 .562 -.889 .036 -.935 -.526+ - .. 046- D 58 16 -11.34 2.5 lA 700. 1.093 -.918 1.014 .707 1.116 -.944 .545 -.989 -.571+ - .. 045- 0 58 15 -16 STEREO PAIR 700. .198 -.890 .872 .. 493 -.578 .814 -.914 .267 -.960 - .. 547+ - .. 046- 0 58 11 -17 .01 2.5 IF 1020. .711 -.974 .858 .401 .722 -1.002 .189 -1.058 -.533+ -.056- D 58 IB -17 .01 Z.5 lA 1020. 1.018 -1.000 1.014 .680 1.037 -1.031 ..441 -I. 085 - .. 596+ -.054- D 58 11-18 STEREO PAl R 1020. .. 864 -.987 .939 .533 -.61B .879 -1.016 .315 -1.072 - .. 564+ -.056-

D 59 -26.23 2.0 2V 620. .OB9 -.899 .. 644 .050 - .. 498 .077 -.918 -.105 - .. 999 -.182- -.081- 0 59 4 -27.65 2.0 2V 600. .386 -.681 .558 .250 -.368 .38't -.702 -.406 -.787 -.790- -.085- D 59 5 .00 2.0 ZV 600. .706 -.232 .530 .. 473 -.155 .723 -.236 -.060 -.265 -a783+ -.029- D 59 -2.83 2.0 2A 600. 1.100 -.669 .912 .691 1.IZ6 -.685 .309 -.719 - .. 817+ - .. 034-

D 63 17 .01 2.0 2V 1000. -.106 - .. 263 .. 209 -.070 -.161 -.106 -.270 -1.682 -.Z63 -1.576- .. 007+ 

~ 0 63 4 16.30 2.5 2V 600. -.339 -1.186 .875 -.225 -.725 -.339 -1.219 -1.929 -1.213 -1.590- .. 006+ 

~ 0 63 5 -36.86 2.5 2F 400 .. .091 -1.283 .910 -.075 .084 -1.3Z6 -1.519 -1.395 -1.603- - .. 069- a 63 6 -36.86 2.5 2A 400 .. .406 -.948 .731 .339 ..409 -.975 -1.241 -1.041 -1.650- - .. 066-

~ 0 63 5- 6 STEREO PAIR 400 .. .249 -1.116 .825 .153 - .. 478 .246 -1.149 -1.380 -1.211 -1.626- -.068-

to 0 64 2 -8 .. 50 1.5 2F 1000. .. 196 -1.381 .989 .083 .190 -1.398 -1.741 -1 .. 4'24 -1.937- - .. 026- ~ ~ to 0 64 3 -9.21 2.0 2A 2000. .009 -.729 .517 .017 .006 -.743 -1.998 -.769 -2.004- -.026-

t-3 0 64 2- 3 STEREO PAIR 1500. .103 -1.055 .790 .063 -.683 .098 -1.073 -1.872 -1 .. 099 -1.970- -.026- 1-1 D 64 6 -17.72 Z.O If 1200. .039 -1.227 .871 -.037 .031 -1.255 -1.969 -1.295 -2.000- -.040- t-3 0 64 7 -17.72 2.0 IA 1200. .367 -.868 .668 .265 .370 -.891 -1.667 -.929 -2.037- -.038- D 64 6- STEREO PAl R 1200. .203 -1.047 .716 .127 -.651 .200 -1.073 -1.818 -I.J lZ -2.018- -.039- D 64 8 2.83 3.0 2F 1000. -.848 -.292 .635 -.535 -.868 -.301 -2.869 -.313 -2.001- -.012- a 64 9 2.83 3. a 2A 1000. -.261 .12l .208 -.165 -.268 .124 -2.313 .1l3 -2.045- - .. 011+ 0 64 8- 9 STEREO PA IR 1000. -.555 -.085 .473 -.357 - .. 064 -.568 -.088 -Z.591 -.099 -2.023- -.011- 0 64 10 2.83 3. a ZV 600. -.570 -.57D .570 -.387 -.3B9 -.580 -.591 -2.617 - .. 603 -Z.031- -.I 12-

Approved for Release: 2018/09/11 C05103025 __________________ _ 
I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

BCS 39739-65 

nApproved for Release: 2018/09/11 C051 03025 .I.~U.L:Jv.I.\ • .L:J J. - U~.l.YU.JJ. J. Handle via Byeman 

Controls Only 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

RE"V 0 it 

ACC. SYSTE,..1 

NO. T Ie.E 

REV 0 

SEC 

4498 .. 09 

4512.19 

4:'21.99 

4607.79 

4620.29 

4172.69 

4185 .. 59 

1 9775.99 

9790 .. 89 

9980.59 

9991 .. 89 

10071.09 

10082.79 

10136.29 

10161.49 

9 10194.39 

10 I021I.69 

11 10225.39 

12 10251.49 

13 10261.99 

14 10280 .. 19 

15 10294.29 

16 10900.89 

17 10912.59 

REV [l 6 

8 

9 

10 

II 

12 

13 

14 

15 

16 

17 

18 

19 

ZO 

REV D 7 

1 

2 

3 

4 

5 

7 

8 

9 

10 

11 

12 

13 

14 

15 

16 

17 

18 

19 

20 

21 

REV 0 8 

1 

2 

3 

10 

II 

U 

13 

14 

1':.> 

16 

l7 

15103.89 

15115.99 

1540 I .. 19 

1541I.89 

15427.99 

15620 .. 69 

15634 .. 39 

l?673.29 

15724.99 

15739.49 

15781.49 

15805.99 

15831 .. 29 

15841 .. 39 

15860 .. 09 

15872.59 

16155.39 

16168~29 

16199.69 

16211.39 

L0363.6R 

20375.38 

20437.48 

20451 .. 58 

20618 .. 88 

20643.18 

20654.88 

20670 .. 68 

L0696.38 

20706.88 

Z0730.38 

20766.88 

20178.58 

20881.58 

ZOB9't. AS 

21066.28 

21078.78 

21308.28 

21318.38 

ZU96 .. 7!) 

Zlft08.88 

25649.88 

25662 .. 78 

25682.98 

25696.28 

25995 .. 78 

26D09.9!::l 

2hO~3. 21-< 

26081. lA 

26097.58 

26160 .. 18 

,zh171.RH 

2h2';:d s 9t-. 

26~70~0;: 

?A/'Ji .. ' ... H 

26314.~;H 

2632U e OB 

?6"HH.5R 

Handle via Byeman 

Controls Only 

8URS T 

T I ME 

SEC 

5.1 

5.1 

5.1 

5.9 ,.9 

6.3 

6.3 

5.9 ,.9 

7.1 

7.1 

6.3 

8.9 

5.4 

6.3 

9.1 

6.3 

6.3 

6.7 

6.7 

6.3 

10.3 

6.3 

6.3 

5.5 ,.5 

6.3 

9.7 

10.6 

5.9 

5.9 ,.1 

5.5 

12.4 

5.3 

14 .. 4 

7.1 

7.1 

5.1 

30.1 

7.5 

7.5 

7.5 

7. ? 

6.3 

6.3 

5. I 

5.1 

5.1 

6.3 

6.3 

;'.1 

6.7 

6.7 

6.3 

6.3 

6.3 

6.7 

6.7 

5.9 

15.8 

7.1 

8.6 

h.7 

6.7 

7.5 

7. , 

5.5 

5.5 

9.0 

0.7 

6.7 

11.0 

5.5 

6.1 

10. b 

">.3 

6.4 

'.3 

6.3 

DEG 

69 

68 

62 

51 

73 

59 

53 

52 

49 

47 

45 

43 

43 

41 

40 

39 

38 

3 

73 

,3 

52 

51 

38 

34 

31 

30 

27 

25 

24 

22 

21 

1 

77 

72 

60 

59 

57 

55 

54 

53 

50 

43 

30 

29 

13 

13 

7 

80 

78 

57 

56 

51 

50 

46 

40 

38 

37 

35 

35 

CO/"MANO pos IT ION 

lAT LONG 

MIN OEG MIN 

56N 

21N 

39N 

31N 

13N 

40N 

33N 

46N 

08N 

25N 

lDN 

59N 

03N 

16N 

33N 

18N 

20N 

22S 

14N 

26N 

42N 

37N 

28N 

52N 

19N 

19N 

26N 

45N 

DIN 

02N 

ION 

42N 

21S 

33N 

54N 

54N 

16N 

25N 

41N 

58N 

23N 

54N 

OON 

Z 6N 

34N 

47N 

05N 

41N 

03N 

07N 

39N 

42N 

52N 

45N 

30N 

42N 

OSN 

'jQN 

27·\j 

:;6r~ 

01:\1 

164 

162 

159 

154 

145 

135 

133 

133 

131 

131 

130 

130 

130 

129 

129 

129 

129 

121 

123 

III 

110 

110 

107 

106 

105 

105 

104 

104 

104 

103 

103 

100 

100 

108 

100 

91 

91 

90 

89 

89 

88 

88 

B5 

83 

83 

80 

80 

79 

94 

88 

68 

67 

66 

65 

64 

64 

62 

62 

62 

62 

61 

19E 

59E 

17E 

49E 

40E 

38E 

16E 

ODE 

54E 

25E 

49E 

31E 

17E 

52E 

42E 

25E 

12E 

58E 

30E 

OlE 

47E 

26E 

02E 

16E 

33E 

22E 

50E 

31E 

13E 

52E 

43E 

33E 

05E 

50E 

52E 

47E 

03E 

16E 

36E 

21E 

48E 

OOE 

53E 

llE 

OlE 

IbE 

IDE 

lBE 

17E 

02E 

09E 

47E 

06E 

45E: 

32E 

20E 

58E 

43E 

23E 

OitE 

52E 

COMMAND INFORMATION 

BEST EPHEMERIS 

LAT LONG 

OEG MIN 

69 56.57N 

69 1.00N 

68 22.26N 

62 39.88N 

61 49.63N 

51 32.15N 

50 39.57N 

73 13.35N 

72 15.65N 

59 40.90N 

58 55.25N 

53 34.10N 

52 46.50N 

49 8.42N 

47 25.48N 

45 10.90N 

44 .06N 

43 3.93N 

41 16.90N 

40 33.82N 

39 19 .. 10N 

38 21.18N 

3 21~65S 

9.895 

73 15.12N 

72 28.30N 

53 26.96N 

52 43.42N 

01 37.86N 

38 29.16N 

37 32.86N 

34 52.90N 

31 ZO.04N 

30 20.30N 

27 27.16N 

25 46. ION 

24 1.70N 

23 20.0 IN 

22 2.81N 

21 1l.20N 

1 43.08N 

o 49.83N 

1 19.73S 

7.99S 

77 33.85N 

76 50.7BN 

72 54.98N 

72 .26N 

60 55.20N 

59 17.15N 

58 29.85N 

57 25.91N 

55 41.7ZN 

54 59.09N 

53 23.57N 

50 54.93N 

50 7.2 IN 

43 5.99N 

42 11.46N 

30 26 .. 72N 

29 35.21N 

13 47.82N 

13 6.09N 

7 42.19N 

6 52.21N 

80 

79 

78 

77 

57 

56 

55 

51 

50 

46 

45 

40 

38 

37 

35 

35 

34 

3.05N 

18.61N 

6 .. 77N 

18.27N 

38 .. 9n~ 

41.43N 

47.49N 

52.06N 

45.22N 

29.55N 

41 .. 68N 

5.13N 

59 .. U2N 

26 .. 9SN 

56. lIN 

.. 5Hi\I 

lL"37N 

DEG 

164 19.95E 

163 31.14E 

162 59.40E 

159 17.96E 

158 52.04E 

154 49.36E 

154 33.15E 

145 40. 76E 

144 30.29E 

135 38.41E 

135 18.42E 

133 16.40E 

133 .56E 

131 53.56E 

131 24.65E 

130 49.00E 

130 31.1IE 

130 17.3ZE 

129 51.87E 

129 41.93E 

129 25.05E 

129 12.26E 

121 57.86E 

121 50.25E 

123 30.30E 

122 32.36E 

III 1.40E 

110 46.96E 

110 25.95E 

107 1.46E 

106 49.240 

106 15.70E 

105 33.37E 

105 21.90E 

104 49.52E 

104 31.16E 

104 12.56E 

104 5.23E 

103 51.78E 

103 42.88E 

100 33.32E 

100 24.95E 

100 4.57E 

99 56.98E 

108 50.31E 

107 13.50E 

100 52.07E 

99 47.3bE 

91 47.52E 

91 2.73E 

90 42 .. 46E 

90 16.27E 

89 36.30E 

69 20.BIE 

8B 47.72E 

88 .IOE 

87 45.69E 

85 52.74E 

85 39.64E 

83 10.62E 

83 .85E 

60 16.34E 

80 9.55E 

79 17.56E 

79 9.62E 

94 

91 

88 

86 

68 

67 

67 

66 

65 

64 

64 

62 

62 

62 

62 

61 

6/ 

14.78E 

33.35E 

.40E 

1~ 54E 

9.05E 

46.36E 

25 .. 97E 

5.42E 

44.67E 

31.99E 

19.40E 

57.85 E 

43.05E 

22.99E 

3.77E 

52.Z8E 

43.47E 

~-GAMBIT 

FILM VELOCITY IN./SEC. MIR- CRAB ROLL ROR 

COMMAND 

2.6899 

2.7168 

2.6840 

2.8840 

2.8840 

2.7991 

2.7714 

2.4841 

2.4841 

3.1229 

3.1541 

3.2497 

3.2822 

3.2175 

3.0920 

3.1857 

2.6899 

2.6633 

3.3482 

3.3817 

2.5089 

2.5594 

3.1229 

3.0614 

3.00 II 

3.0311 

2.4841 

2.4841 

2 .. 4841 

2.5594 

2.6369 

3.0011 

2.5850 

2.6369 

3.1857 

3.5542 

3.5542 

3.5542 

3.1229 

3.1229 

2.7714 

2.7168 

3.1857 

3.1541 

2 .. 9713 

3.0011 

2.6899 

2.7168 

2.8840 

3.0011 

3.0011 

2.4841 

3.2822 

3.2822 

2.7440 

2.9713 

3.00 II 

2.6633 

2.6108 

2 .. 9713 

2.9419 

3.4841 

3.4841 

3.1541 

3.0920 

2 .. 9419 

2.9419 

2.7714 

2.7991 

2 .. 5340 

2.7991 

2 .. 8554 

3.3482 

3.3817 

3.0311 

3.0614 

2 .. 7714 

3.1541 

3 .. 3482 

3.4496 

3.4155 

3. 'd 55 

AC TUAL 

2.690 

2.717 

2.853 

2.884 

2.887 

2.800 

2.774 

2.485 

2.486 

3.124 

3.154 

3.248 

3.283 

3.218 

3.093 

3.187 

2.692 

2.637 

3.345 

3.385 

2.510 

2.558 

3.122 

3.059 

2 .. 999 

3.032 

2.483 

2.486 

2 .. 486 

2.556 

2.636 

3.000 

2.585 

2.634 

3 .. 188 

3.553 

3.553 

3.553 

3.121 

3.121 

2.775 

2.716 

3.1 B7 

3.153 

0.000 

0.000 

0.000 

0.000 

2.887 

3.000 

3.000 

2 .. 486 

3.280 

3.260 

2.742 

2.974 

3.004 

2.663 

2.610 

2 .. 974 

2.943 

3.488 

3.488 

3 .. 151 

3.091 

2 .. 940 

2.940 

2.773 

2.799 

2.533 

2 .. 799 

2.851 

3.348 

3.384 

3 .. 030 

3 .. 060 

2~711 

3.152 

3.152 

3.448 

3 .. 413 

3 .. 416 

pas. DEG. ANGLE 

.5 -29.069 

.5 -29.069 

1.0 -24.106 

2.0 23.397 

2.0 23.397 

2.5 31 .. 196 

2.5 31.196 

.5 -37.577 

.5 -37.577 

1.5 -16.307 

1.5 -16.307 

2.0 -14.889 

2 .. 0 -14 .. 889 

2.0 25.524 

2.0 -24.815 

2.5 19.852 

2.5 36.159 

2.5 36.159 

2.5 -1,.598 

2.5 -15.598 

1.5 -43.958 

1 .. 5 -43.958 

3.5 15.598 

3.5 15.598 

1.0 -9.217 

1.0 -9.217 

1.5 45.376 

2 .. 0 45 .. 376 

2 .. 0 45 .. 376 

1 .. 5 -43 .. 249 

1.5 -43.249 

2.0 34.741 

2.0 -43.958 

2.0 -43.958 

2.5 -36.1,9 

3.0 -25.524 

3.5 .. 709 

3.5 .. 709 

2.5 31.905 

2 .. 5 31 .. 905 

3 .. 0 31 .. 905 

3.0 31.905 

3 .. 5 -19 .. 852 

3 .. 5 -22 .. 688 

.. 5 -1 .. 418 

.5 -1.418 

1.5 26.233 

1.5 26.233 

1 .. 5 -26 .. 9't2 

2.0 21.270 

2.0 21.270 

2 .. 0 40.413 

2 .. 0 4.963 

2.0 4.963 

2 .. 0 -36 .. 868 

1 .. 5 -29.778 

1.5 -29.778 

2.5 37.577 

2 .. 5 37 .. 577 

2s5 32.614 

2 .. 5 32.614 

3.5 0.000 3., 0.000 

3 .. 5 20.561 

3 .. 5 20 .. 561 

.5 

.5 

1.0 

1.0 

1.0 

1.5 

1.5 

2.5 

2.5 

2.0 

2.0 

2.0 

2.5 

3.0 

3.0 

3.0 

3.0 

-4.254 

-1 .. 090 

19.852 

19 .. 852 

-38 .. 995 

-31.905 

-31~905 

3 .. 545 

3.545 

-29 .. 069 

-29.069 

39.704 

22 .. 688 

-20.561 

9.926 

11 .. 344 

11 .. 344 

Approved for Release: 2018/09/11 C051 03025 

A-8 
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~ 

~Appp~ rovee~d for Release: ~ 2018/09/11 C051 03025 ~J.:J'-'.I.\'J.:J.I. - \J..n..LV.l. ....... .I. ... 

BCS 39739-65 

Handle via Byeman 

Controls Only 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Ace. 

NG. 

KEV 0 9 

1 

2 

3 

4 

S 

10 

11 

11 

13 

14 

I' 

16 

17 

18 

1 y 

,u 

21 

22 

23 

24 

t: ~) 

26 

n 

28 

29 

30 

31 

" 

REV [) 10 

s Y STEM 

TIlH: 

SEC 

30964.88 

30979.313 

31012" 18 

31025~88 

31062.98 

31079.08 

31091.58 

31l{l7 .. 08 

31122 .. 88 

31162.48 

31174 .. 98 

31284 .. 48 

31jOO .. 58 

3133t..68 

31347.58 

31384.98 

31400.48 

31412.18 

31427.78 

31443 .. 28 

314~)6e18 

31494.88 

31?14.98 

31530.98 

31541.48 

31S60.98 

31615.48 

31627.98 

31682.48 

31872.48 

31883.38 

31911.28 

1 36266 .. 18 

36279~ 18 

36463.28 

3647':1.88 

36494 .. 28 

36513.88 

36561.88 

36573.98 

9 36592.98 

10 36604.28 

11 36617 .. 48 

12 36629" IB 

13 36646 .. 28 

14 366')tI.08 

i.~J J(,070.58 

16 36688.98 

17 36701.,08 

18 36727 .. 08 

1'1 36744~48 

2036762 .. 58 

7.1 36774.78 

22 36783.98 

23 36800 .. 08 

24 36812.88 

2~ 36847.08 

26 3613)8.38 

27 36882.58 

28 36Bg3.08 

29 37312.88 

30 37321.78 

31 37375.38 

32 37388.68 

33 37426.68 

34 37437.18 

j) 37454.58 

:16 37465~08 

37 37471-LAR 

3H 375~1.18 

39 3756:'.68 

4U .37577.jE; 

k I V [J II 

BuRS r TII'1l 

SeC 

5.5 

6.0 

6.0 

6.3 

7.2 

7.0 

7.8 

5.1 

7.5 

7.5 

7.3 

6.3 

8.2 

10.8 

5.7 

6. 4 

6.4 

6.2 

5.9 

5.9 

5.3 

5.5 

5.5 

5.3 

6.3 

12.9 

5.'1 

6.0 

5.6 

5.7 

6.7 

6.7 

5.9 

5.9 

5. I 

5.1 

7.1 

7.8 

7.8 

5.5 

10 .. tI 9.' 

6 .. .3 

5.5 

5.1 

5.4 

7.9 

22.2 

7.1 

7. I 

6 .. 3 

6.3 

5.5 

5. , 

5.5 

5 .. ':1 

1 416':15.78 7.1 

41':>70.68 15 .. 1 

41HY4~98 :' .. 'J 

41909.48 5 .. :' 

41924 .. 98 5.9 

41939.88 ':1.9 

[tlY~)4.9H 5 .. 3 

421:».80 1.1 

[,216"'.)11 7.1 

Handle via Byeman 

Controls Only 

C[)I>IMAND PUSIT ION 

lAT LONG 

DEG 

80 

78 

74 

73 

7Z 

71 

68 

67 

60 

59 

56 

56 

53 

52 

50 

49 

48 

46 

44 

43 

42 

41 

37 

33 

20 

II 

82 

al 

70 

69 

68 

66 

63 

61 

60 

58 

57 

56 

55 

54 

52 

51 

50 

49 

48 

47 

46 

44 

42 

12 

MIN 

47N 

03N 

54N 

53N 

04N 

03N 

27N 

37N 

18N 

13N 

55N 

03N 

31N 

28N 

37N 

33N 

41N 

03N 

40N 

3SN 

52N 

32N 

48N 

12N 

09N 

28N 

JlN 

32N 

16N 

26N 

14N 

56N 

44N 

39N 

OON 

04N 

16N 

2SN 

I1N 

22N 

36N 

25N 

11N 

21N 

't4N 

38N 

46N 

26N 

OON 

26N 

08N 

36N 

41N 

01N 

57S 

45S 

78 51N 

77 5aN 

63 26N 

61 25N 

')9 24N 

4:' 46N 

DEG MIN 

75 

65 

59 

57 

55 

54 

52 

51 

47 

46 

45 

45 

44 

44 

43 

43 

42 

42 

41 

4 I 

41 

41 

40 

39 

36 

36 

61 

57 

31 

30 

29 

28 

26 

25 

24 

23 

23 

23 

22 

22 

21 

21 

21 

20 

20 

20 

20 

19 

18 

13 

12 

\2 

11 

II 

10 

10 

23 

21 

14E 

39E 

lSE 

43E 

27E 

21E 

DOE 

22E 

06E 

36E 

39E 

19E 

25E 

05E 

30E 

1lE 

56E 

13E 

51E 

35E 

24E 

05E 

15E 

18E 

S5E 

28E 

21E 

03E 

23E 

38E 

37E 

39E 

38E 

32E 

45E 

54E 

35E 

15E 

48E 

30E 

54E 

32E 

09E 

55E 

44E 

25E 

llE 

35E 

59E 

25E 

44E 

10E 

52E 

37E 

50E 

33E 

30E 

OlE 

15E 

I zE 

16E 

17W 

COMMAND INFORMATION 

BEST EPHEMERIS 

LAT LONG 

OEG MIN 

80 

79 

78 

77 

74 

73 

73 

72 

71 

68 

67 

60 

59 

56 

56 

53 

52 

51 

50 

49 

48 

46 

44 

43 

42 

41 

37 

36 

33 

20 

19 

17 

47.34N 

58.96N 

3.50N 

13 .48N 

54.47N 

52.94N 

4.79N 

4.68N 

3.02N 

27.11N 

37 .57N 

18.95N 

13.94N 

55*94N 

3.63N 

31.69N 

28.61N 

40.95N 

37 .36N 

34.12N 

41.45N 

3.25N 

40.97N 

35.42N 

52.39N 

32.42N 

48.63N 

57.25N 

13 .02N 

9.40N 

24.38N 

29.15N 

82 !! .05N 

81 32.18N 

70 15.97N 

69 26.37N 

68 13.65N 

66 55.84N 

63 44.09N 

62 55.53N 

61 39.13N 

60 53.61N 

60 .36N 

59 13.11N 

58 3.95N 

57 16.l7N 

56 25.50N 

55 1O.83N 

54 21.67N 

52 35.90N 

51 25.02N 

50 11.21N 

49 21.42N 

48 43.86N 

47 38.07N 

46 45.74N 

44 25.76N 

43 39.47N 

42 .25N 

41 17 .l8N 

12 26.68N 

11 41.65N 

8 8. 50N 

7 13.56N 

4 36.64N 

3 53.29N 

2 41.46N 

I 58.12N 

1 1.17N 

3 57.025 

4 56.785 

5 44.985 

78 51.76N 

77 58.32N 

63 26.28N 

62 28.04N 

61 25.67N 

60 25.61N 

59 24.65N 

4? 47.02N 

44 50.94N 

DEG 

75 

71 

65 

63 

59 

57 

56 

55 

54 

52 

51 

47 

46 

45 

45 

44 

44 

43 

43 

43 

42 

42 

41 

41 

41 

41 

40 

40 

39 

36 

36 

36 

MIN 

15.1'E 

46.78E 

39.74E 

38.52E 

l'.50E 

43.76E 

39.69E 

27.62E 

21 .. 3SE 

.51E 

22.10E 

5.63E 

36.4>E 

39.56E 

19.55E 

25.54E 

4.68E 

49.46 E 

29.82E 

10.99E 

55.79E 

12.56E 

51.33E 

34.98E 

24.48E 

5.46E 

15.15E 

4.14E 

18.03E 

54.17E 

47.13E 

27 .. 76E 

61 20.77E 

57 2.12E 

31 22.81E 

30 37.74E 

29 37.39E 

28 39.25E 

26 37.90E 

26 11.l2E 

25 31.59E 

25 9.41E 

24 44.62E 

24 23.59E 

23 54.30E 

23 35.00E 

23 15.31E 

22 47.6lE 

22 30.l6E 

21 54.51E 

21 31.93E 

21 9.41E 

20 54.74E 

20 43.93E 

20 25.5lE 

20 11.29E 

19 34.94E 

19 23.41E 

18 59.44E 

18 49.33E 

13 25.47E 

13 18.19E 

12 44.03E 

12 35.30E 

12 10.45E 

12 3.61E 

11 52.29E 

11 45.47E 

11 36.51E 

10 49.55E 

10 40.l!E 

le 32.4qE 

23 31.14E 

21 I. 74E 

4 15.32E 

3 43.94E 

3 12.33E 

2 43.62E 

2 16.03E 

2 16.89W 

2 31 .. 34\1 

~-GAMBIT 

FILM VELOCITY IN./SEC. MIR- CRAB ROLL 

ROR 

COMMAND 

2.5850 

2.6108 

2.6369 

2.6369 

2.9713 

2.7991 

2.8271 

2 .. 7440 

2.7991 

2.9128 

2.9128 

2 .. 4841 

2.4841 

2.7991 

2.8554 

2.94 19 

3.0011 

3.0011 

2.7168 

2.7991 

2.7714 

3.1541 

2.7991 

3.3482 

3.3817 

3.3150 

3.0311 

2.9713 

3.6256 

3.4496 

3.4155 

2.8554 

2.7714 

2.7714 

2.9128 

2.9128 

2.4841 

2.8840 

2.9419 

2.9419 

3.2175 

3.2175 

3.2497 

3.2822 

2 .. 6899 

2.8840 

2.9419 

3.1541 

3.1857 

3.3817 

3.3482 

3.2175 

2.5850 

2.9713 

3.1229 

2.6108 

3.03 I 1 

3.1229 

3.3150 

3.2822 

3.4155 

3 .. 4496 

2.9419 

2.8554 

3.3150 

3.3482 

3.2822 

3.3150 

3.6256 

2 .. 6633 

2.5594 

2.4841 

2.4841 

2.4841 

2.630,9 

2.6108 

2.50B9 

2 .. 4841 

2.4841 

2.6369 

2.5850 

ACTuAL 

2.584 

2.609 

2.635 

2.635 

2.968 

2.798 

2.824 

2. 7'~2 

2 .. 797 

2.911 

2.911 

2.483 

2.4B3 

2.796 

2.854 

2.938 

3.000 

3 .. 001 

2.713 

2.797 

2.771 

3.154 

2.797 

3.346 

3.383 

3.3 15 

3.029 

2.973 

3.624 

3.448 

3.413 

2.855 

2.772 

2.772 

2.911 

2.9 I 1 

2.487 

2.884 

2.938 

2.941 

3.218 

3.218 

3.247 

3.283 

2.691 

2.883 

2.939 

3.151 

3.186 

3.380 

3.344 

3.214 

2.586 

2.969 

3.12l 

2.607 

3.028 

3.120 

3.313 

3.282 

3 .. 414 

3.448 

2.940 

2.851 

3.312 

3.348 

3.282 

3.312 

3.623 

2 .. 661 

2.556 

2.485 

2.486 

2.486 

2.634 

2.608 

2.508 

2.486 

2 .. 486 

2.634 

2 .. 584 

POSe OEG. ANGLE 

1 

1 

1 

1 

2 

1 

1 

2 

2 

2 

2 

2 

2 

2 

2 

2 

1 

I 

2 

2 

2 

2 

2 

2 

2 

2 

1 

1 

2 

I 

1 

2 

2 

2 

2 

2 

1 

2 

1 

1 

1 

I 

1 

I 

2 

2 

2 

2 

2 

2 

2 

2 

2 

2 

2 

2 

1 

1.0 

1.0 

1.0 

1.0 

.5 

.5 

.5 

.5 

.5 

1.5 

1.5 

2.0 

2.0 

1.5 

1.5 

1.5 

2.0 

2.0 

1.5 

2.0 

2.0 

2.0 

2.0 

2.5 

2.5 

2.5 

2.5 

2.5 

2.5 

3.5 

3.5 

3.0 

26 .. 942 

26.942 

26.942 

26.942 

-24.106 

-230397 

-230397 

-25.S24 

-25~524 

200561 

20.56 I 

43 .. 249 

43 .. 249 

-31.905 

-31.905 

33.323 

24.815 

24 .. 815 

36.868 

32.614 

32.614 

-24.815 

-41.83 I 

-14.889 

-14.889 

14.180 

280360 

28.360 

14.180 

9.217 

9.217 

-38.995 

~5 17 .. 725 

.5 IH9434 

1.5 19.143 

1.0 19.143 

.5 43.958 

1.0 22.688 

2.0 21.270 

2.0 21.270 

2.0 5.672 

2.0 5.&72 

1.5 -5.672 

1.5 -5.672 

1.5 -36d';;9 

1.5 -29.069 

2.0 -29.069 

1.5 -19.143 

2.0 -19.]43 

2.0 -21.270 

2.0 -24.106 

2.0 -29.778 

2.0 -42.540 

1.5 -36.868 

2.0 -330323 

2.0 -42.540 

2.0 -29 .. 069 

2.0 -2g. 069 

2.5 1 4 .889 

2.5 14 .. 889 

3.5 -14.180 

3.5 -14.180 

3.0 29.069 

3.0 29.069 

3.5 -17.016 

3.5 -17.016 

3.5 -16.307 

3.5 -16.307 

3.5 -3 .. S45 

3 .. 0 32 .. 614 

3.0 32 .. 614 

1.5 45.376 

0.0 -34.741 

.. 5 -36.15g 

2.0 32.614 

2.0 32.614 

2 .. 0 36.80,8 

2.0 36.868 

1 .. 0 43.249 

2.5 36 .. A68 

2.5 36.868 

Approved for Release: 2018/09/11 C051 03025 

A-9 
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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Ace. 

NO. 

REV 013 

SY Sl cf-1 

T IMI:: 

SEC 

1 53931.28 

2 53944.18 

~:EV D14 

53957 .. 58 

54035 .. 98 

54049.68 

1 58504 .. 37 

2 58517.67 

REV 015 

1 

2 

6 

7 

8 

RfV 016 

63446 .. 67 

63459.57 

63472.37 

63486.87 

63522.17 

63535.47 

63564 .. 67 

63581.57 

63612.47 

BURS T 

TIME 

SEC 

7.5 

7.5 

6.3 

7.1 

7.1 

5.5 

5.5 

5.1 

5.1 

5.5 

5.5 

5.5 

701 

7.0 

100.1 

1 68691 .. 67 24.8 

68747.47 100.1 

68861.27 7.0 

68912.87 7 .. 5 

68923.37 8.6 

68954 .. 97 6 .. 3 

68969 .. 07 7.1 

REV 017 

1 '(5031.67 

REV 019 

REV 020 

75047 .. 37 

84494.67 

84506 .. 77 

3334.57 

3348.27 

3468.87 

3495.87 

3507.17 

3518.97 

3538 .. 87 

3551.77 

3592.27 

10 3604 .. 77 

REV 021 

1 865 4 .97 8666.27 

8814 .. 07 

8830 .. 17 

8951 .. 97 

8962.',7 

8989 .. 97 

9003 .. 57 

9020 .. 87 

10 9049 .. 87 

11 9060.77 

12 96':17 .. 77 

13 9670.27 

14 9689.27 

15 9737 .. 67 

16 9754 .. 57 

17 976':>,,87 

18 9779.97 

5.5 

5.5 

5.5 

5 .. 5 

5.9 

5.9 

5.1 

5.9 

5.9 

5.1 

6.3 

6 .. 3 

5.7 

12. 9 

5.9 

5.9 

5.9 

5.9 

7.0 

9.5 

10.3 

5.3 

6.2 

5.5 

8.4 

5.9 

5.9 

5 .. 3 

6.0 

5.8 

6 .. 3 

COf-lt-lANlJ PUS I T ION 

LAT LONG 

DEG tJiIN 

30 

32 

38 

20 

55S 

425 

005 

SON 

DEG 

60 

60 

61 

47 17N 90 

45 32N 91 

42 OBN 92 

39 13N 92 

38 04N 92 

35 57N 93 

52 56N III 

49 OBN 112 

41 22N 114 

37 50N 115 

37 07N 115 

34 57N 115 

33 59N 116 

16 

64 

70 

61 

59 

58 

57 

53 

52 

71 

60 

51 

50 

48 

47 

46 

44 

43 

325 

56N 

42N 

46N 

5BN 

24N 

04N 

27N 

36N 

07N 

32N 

13N 

30N 

37f\; 

42N 

31N 

32N 

48N 

471\; 

37N 

435 

525 

395 

146 

172 

169 

163 

162 

161 

161 

160 

159 

147 

140 

137 

136 

136 

136 

135 

135 

135 

127 

127 

126 

126 

126 

MIN 

23W 

44W 

50W 

01W 

43W 

1IW 

01W 

42W 

57W 

24" 

14W 

24W 

25W 

12W 

21" 

49W 

OOW 

40W 

32W 

43E 

31E 

39E 

59E 

26E 

07E 

50E 

56E 

43E 

12E 

59E 

26E 

10E 

51E 

ZOE 

09E 

37E 

17E 

45E 

34E 

27E 

COMMAkO INFORMATION 

BEST EPHEMERIS LAT LONG 

OEG MIN 

30 54.815 

31 47.2B5 

32 41.755 

37 59.755 

38 55.195 

20 50 .. 57N 

19 55.65N 

47 17.12N 

46 24.36N 

45 31.97N 

44 32.60N 

42 7.91N 

41 13.34N 

39 13.46N 

38 4.02N 

35 56.98N 

52 55.06N 

49 7 .. 53N 

41 21.61N 

37 49. "ION 

37 6.54N 

34 56.57N 

33 58.54N 

16 32.045 

17 36.415 

64 57.51N 

64 9 .. U6N 

70 42.03N 

69 48 .. 17N 

61 47.04N 

59 58.15N 

59 12 .. '+9N 

58 24.75N 

57 4 .. 14N 

56 1l.82N 

53 27.22N 

52 36.33N 

71 6.52N 

70 22.19N 

60 32.23N 

59 27.21N 

51 12.54N 

50 29.71N 

48 37.43N 

47 41.84N 

46 31.08N 

44 32.35N 

43 47.69N 

2 46.65N 

1 55.07N 

o 36 .. 70N 

42 .. 865 

52.505 

4 39.055 

5 37.125 

DEG MIN 

60 23.00W 

60 33.19" 

60 43.92W 

61 49.91W 

62 2.IOW 

74 1.16W 

H 10.53W 

90 43.34W 

90 57. 52W 

91 1I.25W 

91 26.42W 

92 1.80W 

92 14.61W 

92 41.85W 

92 57.!IW 

93 24.14W 

111 14.75" 

112 24.79W 

114 25.08W 

115 12.61W 

115 21.88W 

115 49.04" 

116 .83W 

146 39.71W 

146 50.45" 

172 30.85W 

172 59.BOW 

169 43.02E 

168 52.BOE 

163 31.26E 

162 39.33E 

162 19.04E 

161 58.65E 

101 25.98E 

161 5.84E 

160 7.24E 

159 50d9E 

147 55.95E 

147 12.13E 

140 42.BIE 

140 13 .. 28E 

137 1l .. 61E 

136 58.52E 

136 25.66E 

136 10.lIE 

135 50.94E 

135 20,J8E 

135 9.02E 

127 36.76E 

127 28.64E 

127 16.31E 

126 44 0 91E 

126 33.93E 

126 26.57E 

126 11 .. 39E 

Handle via Byeman 

Controls Only ~-GAMBIT 

Handle via Byeman 

Controls Only 

FILM VELOCITY IN./SEC. MIR- CRAB ROLL 

ROR 

COMMAND 

2.7440 

2. H68 

2.9128 

2.5850 

2.5850 

2 .. 7714 

2.8271 

2.9128 

2.9713 

2.5089 

2.5594 

2.7168 

2.7714 

3.7355 

3.4155 

3.7728 

3.3817 

3.6985 

3.6985 

3.2497 

3.2822 

3.62'>6 

3.7728 

2.4841 

2.4841 

3.0920 

3 .. 1229 

2.6633 

2.6633 

2.5594 

3.2175 

3.2175 

3.3150 

2.9713 

2.9419 

2.8840 

2.9128 

3.1229 

3 .. 1541 

2.4841 

2.4841 

3.4155 

3.4155 

3.1229 

3.0614 

2.6108 

3.4496 

3.4496 

2.9713 

2.9128 

3 .. 3150 

2 .. 't-841 

2.4841 

2.5594 

2.5089 

ACTUAL 

2.742 

2.715 

2.911 

2.584 

2.586 

2 .. 770 

2.828 

2.910 

2.972 

2.509 

2.556 

2.713 

2.H2 

3.734 

3.415 

3.770 

3.382 

3.698 

3.697 

3 .. 248 

3.282 

3.624 

3.710 

2.486 

2.486 

3.093 

3.121 

2.659 

2 .. 662 

2.557 

3.219 

3.219 

3.319 

2 .. 969 

2.945 

2.889 

2.913 

3.123 

3.158 

2.485 

2.487 

3.415 

3.418 

3 .. 11 q 

3.058 

2.615 

3.453 

3.449 

2.97 Z 

2 .. 917 

3.318 

2.488 

2.488 

2 .. 564 

2 .. 507 

P05. DEG. ANGLE 

2 

2 

2 

2 

2 

3.0 -8.508 

3.0 -8.508 

3.0 0.000 

3.0 -10.635 

3.0 -10.635 

2 .. 5 -39 .. 704 

2.5 -39.704 

2.0 -32.614 

2.0 -32.614 

1 .. 5 -43.249 

1.5 -43.249 

2.0 -38.995 

2.0 -38.995 

2.5 -1.418 

2.5 22.688 

3.0 -.709 

0 .. 0 -6 .. 381 

2.5 -11.344 

2.5 -14.889 

2.5 -24.815 

2.5 -25.524 

2 .. 5 -19.852 

3 .. 0 -.709 

2.5 34.032 

2.5 34.032 

1.5 -17.016 

1.5 -17.016 

1 .. 5 30 .. 487 

1.5 30 .. 487 

1.0 -43 .. 2'+9 

2.0 11.344 

2.0 II .344 

2.0 3.545 

2 .. 0 25.524 

2 .. 0 25857.4 

1.5 -31.905 

1.5 -31.905 

1 .. 0 -2.127 

1.0 -2.127 

2.0 43 .. 9511 

2.0 43 .. 958 

2.5 -1.418 

2.5 -1.418 

2.0 -33.323 

2.5 -29.778 

1.5 -41.122 

2 ~ 4.963 

2.5 4.963 

3.0 24 .. Rl~ 

3 .. 0 24.815 

3 .. 5 .. 709 

2 .. 5 41 .. 831 

2.5 41.831 

3.0 34.741 

3 .. 0 34 .. 741 

A-lO 

Approved for Release: 2018/09/11 C051 03025 
I 

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'T'IApproved for Release: 2018/09/11 C051 03025 U.LJ\..../.Ll.J...:J ~ - \J.c:L.lY.1..1J.l..l. 

BCS 39739-65 

Handle via Byeman 

Controls Only 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

ACC. 

NO. 

REV 1)22 

SYSTEfl 

TIME 

SEC 

1 139;8.77 

2 13971.67 

14008 e07 

4 14019.37 

5 14037.27 

6 14048.97 

7 14162.97 

B 14177~87 

9 14275.07 

10 14285.97 

11 14432.17 

12 14444 .. 67 

13 14461 .. 97 

14 14473.27 

1::' 14497 .. 37 

16 14548.17 

17 14593.37 

18 14654.07 

19 14673.27 

20 14693 .. 97 

Ll 14714.57 

22 14733 .. 17 

2] 14753.67 

;':4 15058.87 

25 15069 .. 77 

26 15091.97 

ReV ll23 

1 19719.87 

19250 .. 57 

19264 .. 67 

19294.87 

i9523 .. 27 

19537.7"1 

19749.07 

19759.57 

19921 .. 36 

10 19941 .. 77 

11 19964 .. 67 

RfV D24 

1 2449h .. 76 

24?lO .. 46 

24S31 .. 86 

24543 .. 56 

24636.46 

2'1 '~S,~~'):-

24861.1& 

24874 .. 46 

24928.16 

10 24g4I .. 06 

11 24968 .. 66 

12 24983 .. 66 

13 24994 .. 56 

14 25040 .. 46 

I? 25053 .. 76 

16 25072.76 

17 25111.86 

18 25710 .. 76 

19 25220.86 

20 25962 .. S6 

21 25974 .. 66 

Handle via Byeman 

Controls Only 

t'>UR.~ T 

T I ME 

SEC 

&.7 

7.0 

5.9 

5.9 

6.3 

6.3 

7.1 

7.1 

&.7 

&.7 

5.9 

9. I 

'> .9 

9.1 

5.3 

5.3 

'>.3 

5.3 

5.8 

5.3 

5.1 

5.3 

6.7 

&.7 

6.7 

7.2 

5.0 

8.9 

9.3 

5.0 

6~7 

8.7 

6.3 

6.3 

5.6 

11.7 

14.1 

8.3 

8.3 

0.3 

6.3 

5.1 

s. l. 

1:1 .. 6 

10.8 

6.8 

R .0 

5.1 

'>.5 '.5 

5.5 

14.8 

13.8 

6.2 

5 .. 9 

5.9 

6.7 

60-' 

DEG 

72 

71 

69 

67 

59 

51 

40 

39 

38 

37 

36 

32 

29 

25 

24 

22 

21 

20 

18 

2 

4 

76 

74 

73 

71 

56 

55 

41 

29 

28 

26 

77 

71 

50 

55 

51 

50 

48 

47 

43 

42 

41 

38 

32 

19 

COi"lMAN[) POS I T ION 

LAT LONG 

/oliN 

35t< 

45N 

22N 

26N 

02N 

26N 

't3N 

52N 

41N 

55N 

15N 

46N 

40N 

30N 

liN 

45N 

20N 

03N 

39N 

215 

375 

45N 

50N 

S6N 

59N 

46N 

47N 

24N 

35N 

liN 

36N 

44N 

39N 

OON 

OON 

06N 

27N 

34N 

42N 

40N 

48N 

53N 

35N 

55N 

08N 

305 

DEG 

IZ7 

126 

124 

122 

117 

liS 

112 

1I2 

ltl 

til 

III 

ltD 

109 

109 

108 

108 

108 

108 

107 

104 

104 

111 

lOS 

106 

104 

94 

94 

90 

87 

87 

87 

97 

91 

81 

72 

71 

70 

70 

69 

69 

68 

68 

68 

67 

66 

57 

MIN 

22E 

25E 

06E 

33E 

50E 

04E 

13E 

02E 

46E 

36E 

15E 

32E 

56E 

10E 

56E 

41 E 

26E 

l3E 

59E 

37E 

15E 

44E 

15E 

55E 

28E 

43E 

20E 

IDE 

43E 

27E 

10E 

44E 

33E 

13E 

I3E 

53E 

40E 

24E 

51E 

34E 

33E 

20E 

DIE 

25E 

DOE 

26E 

COMMAND INFORMATION 

BEST EPHEMERIS 

LA T LONG 

DEG I.;}N 

72 35.49N 

71 45.29N 

69 22 .40N 

68 37.73N 

67 26.73N 

66 40 .. 18N 

59 2.19N 

58 1 .. 89N 

51 26.85N 

50 42.40N 

40 43.96N 

39 52.64N 

38 41.58N 

37 55.14N 

36 16.05N 

32 46 .. 99N 

29 40.77N 

25 30.46N 

24 11 .. 24N 

22 45.81N 

21 20.78N 

20 3.99N 

18 39.34N 

2 20.49S 

3 5.415 

4 36.875 

76 45.33N 

74 49.74N 

73 55.79N 

71 58.90N 

56 46.02N 

55 47.17N 

41 24.06N 

40 40.97N 

29 35.28N 

28 !t.18N 

26 36 .. 75N 

79 43.92N 

78 5& .. 06N 

77 39.00N 

7& 55.94N 

71 .09N 

70 <t .. 72N 

55 59.89N 

55 5.87N 

51 27.28N 

50 34 .. 66N 

48 41.96N 

47 40.65N 

46 56.07N 

43 48.12N 

42 53.59N 

41 35.66N 

38 55. liN 

32 8.24N 

31 26.64N 

19 29.665 

20 19.185 

OEG MIN 

127 22.30E 

12& 24.76E 

124 5.45E 

123 27.87E 

122 32.82E 

121 59.47E 

117 50.18E 

117 24.79E 

ItS 3.90E 

114 50.2IE 

112 D.llE 

112 1.43E 

111 45.60E 

111 35.4bE 

111 14,34E 

110 31.78E 

109 55.81E 

109 9.76E 

108 55.65E 

108 4D.65E 

108 25.93E 

108 12.79E 

107 58.47E 

104 36.37E 

104 29.30E 

104 14.87E 

111 43.81E 

108 l' ... 40E 

106 54.19E 

104 27.59E 

94 42.40E 

94 20.12E 

90 10.30E 

90 .33E 

87 42.69E 

87 26.97E 

87 9.65E 

97 44 .. 00E 

95 3.00E 

91 32.39E 

89 54.21E 

81 12.85E 

AO 19.17E 

72 12.83E 

71 53.03E 

70 39.88E 

70 23.72E 

69 5D.67E 

69 33.50E 

69 21 .. 36E 

68 32.86E 

68 19.53E 

68 .98E 

67 2't..4&E 

66 .04E 

65 51.94E 

57 25.56E 

57 17.12E 

~T-GAMBIT 

FILM VELOCITY IN./SEC. MIR- CRA8 ROLL 

ROR 

COMMAND 

2.8271 

2.8554 

3.1541 

3.1857 

3.0311 

3.03Il 

2.4841 

2.4841 

3.2175 

3.1857 

2.9713 

2.9419 

3.1541 

3.1541 

3.7355 

2.7714 

3.6619 

2.9713 

3.4155 

3.6256 

3.2175 

2.5850 

2 co 6369 

3.2497 

3.1857 

2.6899 

2.7714 

2.5340 

2.5594 

3.1857 

2 .. 5089 

2.5594 

3.4155 

3.4841 

3 .. 0920 

2.6899 

3.1541 

2 .. &633 

2.6369 

3.0011 

3.0311 

2.7168 

2.6899 

2.8271 

2.8271 

2.6633 

2.7168 

3.0311 

3.4155 

3 .. 4't9& 

2.8554 

2.8271 

3.0920 

2.9419 

3 .. 5542 

3.5542 

2 .. 9419 

2.9128 

ACTUAL 

2.827 

2.852 

3.152 

3.187 

3.033 

3.029 

2.487 

2.488 

3.216 

3.18& 

2.969 

2.937 

3.153 

3.152 

3.731 

2.766 

3.659 

2.970 

3.413 

3.624 

3.216 

2.581 

2.633 

3.249 

3.183 

2.688 

2.776 

2.536 

0.000 

3.191 

2.511 

2.559 

3 .. 419 

3.490 

3 .. 093 

2.690 

3 .. 151 

2 .. 666 

2.639 

3.003 

3.035 

2.720 

2.693 

2.827 

2.827 

2.662 

2.721 

3.031 

3.418 

3 .. 449 

2.853 

2.829 

3.089 

2.945 

3 .. 55& 

3.554 

2.942 

2 .. 916 

POS. DEG. ANGLE 

1.5 23,397 

1 .. 0 24 .. 106 

1.5 4.254 

1.5 4.254 

1.5 17.725 

1.5 17.72S 

2.0 40.413 

2 .. 0 40.'+13 

2.5 17.71:' 

2.5 17.725 

2.5 30.487 

2.0 11.196 

2.5 .'24.106 

2 .. 5 ~4.10& 

2 .. 5 6.381 

2 .. 0 -44.667 

3.0 -19.143 

2.5 35.450 

3.0 11.762 

3.0 -20.561 

3.0 20.501 

2 .. 0 43.95K 

2 .. 0 43.249 

3.5 5.672 

3.5 5.672 

2.5 30 .. 487 

.. 5 -32.614 

1.5 33 .. 323 

.5 13.323 

1 .. 0 -19.143 

1.0 -41.122 

1 .. 5 -4}.R31 

2.5 -14.180 

2.5 -14.180 

2.5 34.741 

2 .. 0 43.249 

2.5 31.196 

000 -26.942 

0 .. 0 -30.487 

.5 -10.1»5 

.5 -10.635 

la5 29.069 

1.5 ~9.0hY 

2 .. 0 30. 'tl3"/ 

1 .. 5 ,0 _'tA 7 

1 .. 5 -38 .. 995 

2.0 -39.704 

2.0 -29.069 

2.5 -9.217 

2.5 -9.?17 

2.5 32.61't 

2.0 33.323 

2.0 32.614 

2 .. 0 -40 .. 413 

3 .. 0 -8 .. 508 

3 .. 0 -8 .. ~08 

3 .. ~) 1..418 

3.5 1.418 

Approved for Release: 2018/09/11 C051 03025 

A-ll 
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T~ 

Approved for Release: 2018/09/11 C051 03025 uJ..:.J ...... .I.\,J..:.J.I. - '-X~lVJ.J.J.I..1. 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

COMMAND INFORMATION 

Handle via Byeman 

Controls Only 

ACC. SYSTEM 

TIME 

8UR5T 

TIME 

cm",MAND POSITION 

LAT LONG 

BE5T EPHEMERIS FILM VELOCITY IN./SEC. MIRRDR CRA8 ROLL 

NO. 

REV 025 

4 

5 

6 

7 

8 

9 

10 

11 

12 

13 

14 

15 

16 

17 

18 

19 

20 

21 

22 

23 

24 

25 

26 

27 

28 

29 

30 

31 

32 

33 

34 

35 

36 

37 

38 

39 

40 

41 

42 

'.3 

44 

RE \/ 1)26 

SEC 

29814 .. 16 

29B27 .06 

29860.66 

29872.36 

29885.86 

29972.66 

30014.96 

30132.86 

30145.76 

30181.46 

30192.76 

30213.96 

30236.26 

30248.76 

30287.96 

30300.46 

30357.16 

30370.86 

30382.46 

30405.96 

30425 .. 46 

30436.36 

30'+79.96 

30490.86 

30510.76 

30521.26 

30541.16 

30736.46 

30753.26 

30864.36 

30877.66 

30934.86 

30947 .. 36 

31065.36 

31081.46 

31218 .. 36 

3]230 .. 86 

31249 .. 06 

31261.56 

31283.56 

31296 .. 06 

31339 .. 86 

31353 .. 96 

31388.06 

I 35J07.06 2 15119 .. 96 

35135 .. 56 

35308.76 

35321.26 

35345 .. 86 

35374 .. 5A 

35388.26 

35425.96 

10 35439 .. 16 

11 35449 .. 66 

12 35470.76 

13 35484.46 

14 35495 .. 46 

15 35505 .. 86 

1(' .:\5542 .. 46 

17 35552.96 

le 35573.66 

1'01 355137.':>6 

20 35599 .. 66 

21 356]2.06 

22 35641.46 

l3 35664 .. 76 

24 3':5677 .. 16 

2~} "15695 .. 46 

L6 35104 .. 8b 

27 3~117 .. 06 

78 35727 .. 56 

79 "i62':>1.36 

30 36268.26 31 36j43 .. 76 

32 16355 .. 06 

33 ::;638.~.16 

j4 3<">593 .. LI6 

3':> .3{'-.426 .. 16 

3/) 3(,430 .. 66 

3-1 j()f-l71:l. f-lo 

::'8 3A491.76 

:s9 :.6502.46 

40 3t>~J14 .. 96 

41 36539 .. 56 

it! 3b":>~Jl.20 

Handle via Byeman 

Controls Only 

SEC 

5. I 

5.1 

6.3 

6.3 

5. I 

5.6 

5.2 

6.3 

14.7 

5.9 

7.9 

5.5 

7.1 

7.0 

7.1 

11o ' t 

7.6 

8.3 

6.6 

5.3 

5.5 

5.5 

5.5 

5.5 

6.3 

6.3 

5.3 

5.3 

5.3 

6.7 

6.7 

5.9 

5.9 

5.9 

5.9 

7. J 

7.1 

5.9 

5.9 

1.6 

7.2 

6.3 

6.3 

7.1 

5.9 

6.3 

5.6 

9.0 

9.0 

6.3 

5.9 

5. 9 

5.3 

6.3 

6.3 

5.9 

6.0 

5.3 

5.6 

6.3 

6.3 

5.3 

5.5 

5.9 

16.7 

lJ.2 

5.1 

6.8 

5.1 

5.1 

7.2 

5.4 

(,.7 

0.7 

5.9 

5.9 

7.1 

10.9 

" .9 

5.9 

~. ~ 

5.5 

9.2 

9.6 

6.3 

".3 

DEG 

80 

75 

70 

67 

59 

58 

56 

55 

54 

52 

51 

49 

48 

44 

43 

42 

41 

39 

36 

33 

31 

18 

17 

9 

14 

16 

19 

19 

22 

26 

82 

81 

80 

69 

68 

67 

65 

61 

61 

58 

58 

57 

56 

5'. 

53 

51 

51 

50 

49 

47 

45 

44 

43 

43 

'.2 

41 

3 

4 

lU 

11 

12 

14 

MIN DEG 

16N 

32N 

58N 

23N 

36N 

43N 

51N 

26N 

40N 

14N 

43N 

53N 

13N 

21N 

29N 

33N 

46N 

09N 

49N 

05N 

5BN 

53N 

28N 

IBN 

39N 

48N 

105 

395 

455 

065 

575 

565 

J35 

02N 

23N 

32N 

lt5N 

55N 

18N 

23N 

57N 

04N 

56N 

01N 

16N 

34N 

05N 

22N 

SoN 

01N 

12N 

21N 

21N 

lt6N 

55N 

40N 

02N 

12N 

28N 

29N 

525 

3J5 

]75 

325 

075 

4':i~ 

::; 75 

185 

77 

69 

65 

58 

56 

51 

51 

50 

49 

49 

48 

48 

47 

47 

46 

46 

46 

45 

45 

44 

44 

43 

41 

41 

39 

39 

37 

36 

35 

35 

35 

34 

34 

64 

60 

56 

35 

34 

33 

32 

30 

29 

28 

28 

28 

28 

27 

26 

26 

26 

25 

25 

25 

24 

24 

24 

23 

23 

23 

17 

16 

14 

MIN 

39E 

04E 

48E 

25E 

04E 

32E 

09E 

liE 

54E 

23E 

52E 

36E 

47E 

33E 

31E 

17E 

06E 

43E 

24E 

36E 

10E 

45E 

ZOE 

09E 

54E 

08E 

43 E 

02E 

17E 

09E 

38E 

03E 

5BE 

50E 

37E 

37E 

54E 

3BE 

20E 

24E 

57E 

59E 

36E 

18E 

02E 

OBE 

53E 

26E 

08E 

53E 

38E 

04E 

39F. 

26E 

07E 

57E 

45E 

35E 

02E 

02E 

HE 

30E 

08E 

34E 

lSE 

IDE 

53E 

LAT LONG 

DEG MIN 

BO 14.77N 

79 30.64N 

77 30.43N 

76 47.25N 

75 56.80N 

70 21.B4N 

67 34.61N 

59 41.65N 

58 49.48N 

50 24.B2N 

55 38.94N 

54 12.7BN 

52 42.01N 

51 51.0BN 

49 11.12N 

4B 20.04N 

44 2B.OIN 

43 31.86N 

42 44.30N 

41 7.88N 

39 47.82N 

39 3.05N 

36 3.81N 

35 18.97N 

33 57.07N 

33 U.B4N 

31 51.B9N 

18 26.23N 

17 16.86N 

9 38.06N 

8 43 ol4N 

4 47.02N 

3 55.44N 

4 11.065 

5 17.365 

14 40.095 

15 31.375 

16 45.995 

17 37.225 

19 7.325 

19 58.495 

22 57 .. 595 

23 55.185 

26 14.345 

82 1.66N 

81 22.41N 

80 32.02N 

69 44.30N 

68 54.94N 

61 17 .. "37N 

65 22.91N 

64 28.08N 

61 56.63N 

61 3.44N 

60 21.07N 

58 55.79N 

58 .3 3N 

57 15.76N 

56 33.58N 

54 4 .. 87N 

53 22.14N 

51 57.83N 

51 1 .. 15N 

50 1l.78N 

49 21.15N 

47 20.98N 

45 45.64N 

44 5't .86N 

43 39.87N 

43 1 .. 33N 

42 11 .. 29N 

41 28.21N 

5 28.50N 

18.76N 

52.645 

39.225 

30.895 

4 17.435 

6 32.06S 

7 23.505 

10 7.175 

11 1 .. 83$ 

11 45.795 

12 37.135 

)4 18.115 

15 6.1]S 

DEG MIN 

77 32.76E 

74 44.9lE 

69 .20E 

67 24.07E 

65 44.86E 

58 23.40E 

56 2.54E 

51 31.37E 

51 B.S9E 

50 ]0.26E 

49 53.08E 

49 22.30E 

48 51.76E 

48 35.37E 

47 47.02E 

47 32.47E 

46 30.80E 

46 16.84E 

46 5.27E 

45 42.48E 

45 24.19E 

45 14.19E 

44 35.62E 

44 26.31E 

44 9.6lE 

44 .95E 

43 44.80E 

41 20.0BE 

41 8.47E 

39 53.70E 

39 44.93E 

39 7.46E 

38 59.32E 

37 42.70E 

37 32.22E 

36 1.75E 

35 53.30E 

35 40.93E 

35 32.37E 

35 17.l9E 

35 8.49E 

34 37.53E 

34 27.38E 

34 2.43E 

64 55 .. 71E 

60 48.38E 

56 35 .. 46E 

35 36.7SE 

34 54.00E 

33 37.87E 

32 20.15E 

31 46.54E 

30 Z3.54E 

29 57.28E 

29 37.28E 

28 59.26E 

2B 35.98E 

28 IS.0IE 

28 1.57E 

27 7.51E 

26 52.9BE 

26 25.45E 

26 7.73E 

25 52.HE 

25 37.85E 

25 4.0ZE 

24 38.59E 

24 25.5lE 

24 6 .. 72E 

23 57.29E 

23 45 .. 27E 

23 35.12E 

17 1.85E 

16 50.83E 16 1. 79E 

15 54.46E 

15 36.86E 

15 29.52E 

15 8.20E 

15 .03E 

14 33 .. 87E 

14 25.{HE 

14 17.97E 

14 9.65E 

13 53.17E 

13 45.2BE 

~GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

COMMAND 

2.9419 

2.9713 

3.0311 

3.0614 

3.0920 

2.6633 

2.7714 

2.9128 

2.9419 

3.1857 

3.2175 

3.2822 

2.8271 

2.8840 

2.8840 

2.9128 

2 .. 5594 

2 .. 610B 

2.1440 

3.6985 

3.5190 

3.5190 

3.5190 

3.5190 

3. 5J 90 

3.5190 

2.8840 

2.7't40 

2.6369 

2.7440 

2.7991 

3.1229 

3.0614 

2 .. 4841 

2.4841 

2.8271 

2.8554 

2 .. 8554 

2.8554 

2.9128 

2.9128 

2 .. 5 594 

2.5089 

2.4841 

2.8554 

2.13 5'54 

3.03]1 

2.9128 

2.9419 

3.3150 

2.6633 

2.6633 

3.4841 

3.3150 

3.3150 

2.7168 

2 .. 7440 

2.5340 

2.8271 

3.3817 

3.4)55 

3.3817 

3.1541 

3.1229 

3.0011 

2.7168 

3.0311 

3.1229 

3.5897 

3 .. 2 49 7 

3.1229 

3.D311 

2.4841 

2.4841 

3.2497 

3.2175 

3.2175 

3.2175 

2.8271 

2.8~54 

2.8271 

2 .. 0554 

2.8271 

2.8~54 

3 ~ 0614 

1.0311 

AC TUAL 

2.944 

2.975 

3.030 

3.058 

3.094 

2.662 

2.772 

2.914 

2.941 

3.169 

3.21B 

3.2B6 

2.892 

2.885 

2.885 

2.912 

2.556 

2.608 

2.742 

3.700 

3.518 

3.520 

3 .. 521 

3.5)9 

3.519 

3.519 

2.886 

2 .. 744 

2.638 

2.145 

2.801 

3.123 

3.061 

2.488 

2.485 

2 .. 830 

2 .. 855 

2.855 

2 .. 854 

2.914 

2.914 

2.560 

2 .. 510 

2.489 

2.855 

7 .. 854 

3.033 

2.917 

2.941 

3.320 

2.660 

2.660 

3.485 

3.319 

3.315 

2 .. 716 

2.743 

2.535 

2.826 

3 .. 386 

3.417 

3.382 

3.156 

3.125 

3 .. 005 

2.718 

3 .. 031 

3.123 

3.594 

3.245 

3.122 

3.031 

2.489 

2.489 

3.248 

3.219 

3.219 

3.219 

2.825 

2 .. 854 

2.831 

2.853 

2 .. 829 

2.853 

3.059 

3.030 

P05. 

2 

2 

2 

2 

2 

2 

2 

2 

2 

1 

1 

I 

1 

J 

I 

2 

2 

2 

I 

I 

I 

OEG. ANGLE 

.5 12.053 

.5 12.053 

1.0 5.672 

1.0 5.672 

1.0 4.254 

1.0 38.286 

1 .. 0 -36.868 

1 .. 5 -29.069 

1 .. 5 -29.069 

1 .. 5 -19 .. 143 

1.5 -19.143 

2.0 12.762 

1.5 -34.032 

1.5 -34.032 

1.5 -33.323 

1 .. 5 -33 .. 323 

[,5 -4I.R31 

1.5 -'+ 1. 831 

2.5 -40.413 

2.5 7.090 

3.0 [.418 

3 .. 0 1.,'+18 

3.0 -7 .. 090 

3 .. 0 -7.090 

3.0 2.127 

3.0 2.127 

2.0 32.614 

2.0 41.122 

2.0 42 .. 540 

2 .. 5 -1R.495 

2.5 -38.995 

3 .. 5 19.143 

3.5 19.143 

2.5 41.122 

2.5 41.122 

3.0 -2't. 106 

3 .. 0 -24.106 

3.5 -21.270 

3.5 -21.no 

3.5 -11.344 

3 .. 5 -11.'.:1,44 

3.0 24.106 

3.0 24.106 

3 .. 0 -lH .. ?H6 

.. 51? .. 0 16 

.. 5 17.016 

.. 5 't.254 

1.0 -23.397 

1 .. 0 -?1.397 

l.() -lh. ~(17 

] .. :' 3,~ .614 

l..5 32.61~ 

1 .. 5 5.f. 12 

2.0 -1.418 

2.0 -1.418 

1.0 -}5 .. 4:'0 

1.0 -35.4':>0 

1.5 -It 1 .. R:4, J 

1.5 -3H.':lY5 

2 .. 0 -4.?",4 

2.0 -4.754 

2.5 5.672 

2.5 11.270 

2.5 21.210 

2 .. 0 2o .. ~33 

1 .. ~ 41..122 

2.0 26.942 

2.0 n.391 

2 .. 5 13.471 

2.5 lR.434 

200 24.106 

2.0 27.651 

2.5 4'-J.376 

2 .. 1j t+5 .. 376 

3.5 8.508 

3.5 8 .. 508 

3.5 -1?053 

3.5 -12.053 

3 .. 0 -29.778 

3.0 -29 .. 778 

3&0 -2706')1 

3.0 -27.651 

3 .. 0 -25.524 

3.0 -25 .. 524 

3 .. 5 -11.344 

3 .. 5 -11&344 

A-12 
I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

~ 

'T'Approved for Release: 

~ 

2018/09/11 C051 03025 U..L.J'-"...L.\.o.A.....l..L - '-AJ.;LJ,.Y.LL.J.&...L 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

COMMAND INFORMATION 

Handle via Byeman 

Controls Only 

Ace .. SYSTEM 

TIME 

BUR 5T 

TIME 

COMMAND POS IT ION 

LAT LONG 

BEST EPHEMERIS FILM VELOCITY IN./SEC. MIRROR CRAB ROll 

NO. 

REV D27 

1 

2 

3 

9 

10 

11 

12 

13 

14 

15 

REV D29 

SEC 

40632 .. 46 

40648 .. 16 

40&57.46 

40671.5& 

40737 .. 36 

40750.66 

40768 .. 2& 

40782.56 

40795 .. 86 

40941.26 

40952.56 

'-tl145.16 

41156.86 

41211.66 

41224.16 

SEC 

5.5 

5.5 

6.3 

6.3 

6.7 

6.7 

5.3 

5.5 

5.5 

7.1 

7.1 

b.3 

6.3 

5.9 

5.9 

1 52810.66 7.1 

7.1 

6.3 

6.3 

2 52824.3& 

Rl=V D31 

52855.46 

5287 I .96 

1 62334 .. 15 

62344.75 

62355 .. 65 

62390 .. 95 

62401.05 

62424.55 

5.0 

5.5 

5.5 

5 .. 9 

5.8 

100.1 

REV 0::52 

1 67526.95 24.8 

2 61582.75 100.1 

3 67717,15 7.0 

67766 .. 65 6.7 

677"ll .. 55 6.7 

67809.35 7.1 

67826.55 5.1 

REV U33 

1 73867 .. 25 5.5 

2 73882.95 5.5 

Rf-V Ol4 

1 77937 .. 55 100.0 

78620.25 5.9 

7863U .. 35 5.9 

RE:V 036 

1 2158.05 6.3 

2169.75 6,3 

2231.65 5.1 

2243 .. 35 ~)~l 

2291 .. 65 5.5 

2304.95 5.5 

2373 .. 65 7.5 

2388.95 7.5 

ReV 037 

1 7504 .. 14 5.5 

7521.04 5.5 

7&36.24 5.1 

4 7649.14 5.1 

5 7735.84 5.3 

7765.84 5.3 

7768.64 7.1 

7799.94 6.9 

7830.44 6.0 

10 7843 .. 74 6.0 

11 8::'88 .. 44 b.Ll 

Handle via Byeman 

Controls Only 

DEG MIN DEG 

69 

68 

62 

60 

59 

49 

35 

30 

34 

37 

43 

42 

39 

38 

36 

56N 

17N 

58N 

54N 

56N 

liN 

14N 

41N 

075 

095 

ION 

27N 

17N 

36N 

59N 

52 14N 

48 26N 

39 15N 

35 52N 

32 56N 

31 45N 

17 235 

6B 19N 

21 53N 

21 liN 

70 liN 

65 19N 

61 IBN 

55 46N 

68 44N 

59 55N 

53 lIN 

51 09N 

49 35N 

48 49N 

46 45N 

4, 50N 

5 185 

13 

12 

o 

56 

56 

87 

B7 

B7 

88 

88 

106 

107 

110 

110 

111 

111 

142 

143 

157 

158 

174 

170 

Ib8 

165 

150 

145 

142 

142 

141 

141 

140 

140 

131 

MIN 

35E 

liE 

44E 

40E 

14E 

23E 

OlE 

53W 

11W 

54W 

01W 

11W 

55W 

04W 

25W 

42W 

50W 

07W 

51" 

27W 

41W 

OIW 

llW 

52," 

OOW 

02E 

19E 

05E 

45E 

35E 

15E 

39E 

OOE 

32E 

IBE 

44E 

30E 

10E 

LAT LONG 

DEG 

69 

68 

6B 

67 

62 

62 

60 

59 

59 

49 

48 

35 

34 

30 

29 

34 

35 

37 

38 

43 

42 

41 

39 

38 

36 

MIN 

56.28N 

54.31N 

17 .. 4BN 

21.50N 

58.33N 

4.82N 

53.89N 

56.16N 

2.40N 

11.05N 

24.B8N 

14.75N 

26.60N 

40.92N 

49 .. 40N 

7.305 

2.855 

8.815 

15.555 

10.43N 

26.95N 

42 .. 24N 

17 .30~ 

35.BIN 

59.21N 

52 13. 39N 

48 25.63N 

39 14.80N 

35 51.31N 

35 6.47N 

32 55.57N 

31 44.74N 

17 23.335 

18 27.625 

68 19.43N 

21 52.72N 

21 11.03N 

70 1l.54N 

69 25.41N 

65 19.23N 

64 32.38N 

61 IB.!7N 

60 24.50N 

~5 46.19N 

54 44.00N 

68 44.63N 

67 37 .. 57N 

59 55.34N 

59 3.!7N 

53 11.14N 

51 8.85N 

49 35 .. 78N 

48 49.61N 

46 44.88N 

45 50.44N 

5 17.925 

OEG 

13 

12 

12 

11 

8 

8 

7 

7 

o 

o 

a 

I 

56 

56 

56 

57 

87 

87 

87 

87 

88 

88 

MIN 

35.55E 

41.40E 

1l.47E 

28.80E 

43.67E 

15.59E 

40.59E 

13.76E 

49.98 E 

22.78E 

9.60E 

1.16E 

8.70W 

53.21W 

3.02W 

16.55W 

27.91H 

54.39W 

8.85W 

1.07W 

1l.56W 

22.16W 

55.29W 

4.46W 

25.33W 

106 42.11W 

107 50.52W 

110 7.71W 

110 Sl.A8H 

III .76W 

III 27017" 

III 41.07W 

142 1.48W 

142 12.27W 

143 10.66W 

157 52.58W 

157 59.76" 

174 2.70E 

173 20.97E 

170 18.82E 

169 50.11E 

168 5.44E 

167 39.90E 

165 44.77E 

165 22.25E 

150 34.79E 

149 42.l7E 

145 14.97E 

144 51.91E 

142 38.B2E 

141 59.63E 

141 31 .. 66E 

141 18.31E 

140 43.81E 

140 29.40E 

131 9.63E 

~-GAMBIT Approved for Release: 2018/09/11 C051 03025 

COMMAND 

2.4841 

2 .. 48'tl 

2.6108 

2.610B 

2.6633 

2.6899 

2.6899 

2.8271 

2.8840 

3.1541 

3.1B57 

3.[229 

3.0920 

2.8554 

2.9128 

2.6369 

2.6108 

2.4841 

2.4841 

3.4155 

3.3817 

3.4155 

3.5190 

3.5190 

3.8106 

3.3817 

3.7728 

3.8106 

3.3817 

3.4155 

3.8106 

3.2822 

2 .. 4841 

2.4841 

2.8554 

3.5190 

3.5190 

2.9713 

3.0011 

3.2497 

3.2822 

2.7991 

2.7991 

2.4841 

2.5089 

2048'd 

2.4841 

2.9128 

2.9419 

2.8554 

3.6985 

3 .. 0614 

3.0920 

2.8211 

2.7714 

2.4841 

ACTUAL 

2.486 

2.486 

2.611 

2.611 

2.659 

2.693 

2.693 

2.829 

2.886 

3.152 

3.192 

3.123 

3.094 

2.850 

2.911 

2.637 

2.610 

2.488 

2 .. 487 

3.419 

3.383 

3.415 

3.519 

3.529 

3.814 

3.380 

3 .. 776 

3.810 

3.386 

3.416 

3.810 

3.283 

2.483 

2.487 

2.854 

3.519 

3.515 

2.972 

3.004 

3.249 

3.284 

2.800 

2.800 

2 .. 489 

2.507 

2.487 

2.483 

2.912 

2.942 

2.849 

3.700 

3.059 

3.092 

2.825 

2.770 

2 .. 485 

POS. DEG. ANGLE 

1.5 38.995 

1.5 3B.995 

1.5 33.323 

1.5 33.323 

1.0 -35.450 

1.0 -35.450 

1.0 -35.450 

1.0 -31.196 

1.0 -31.196 

2.0 -24.815 

2.0 -2't.815 

2.5 26.233 

2.5 26.233 

2.5 -37.577 

2.5 -37.577 

3.0 2.836 

3.0 2.836 

2.5 -29.069 

2.5 -29.069 

2 .. 5 -26.942 

2.5 -15.598 

2 .. 5 -15.598 

3.0 -2.836 

3.0 -2.836 

3.0 -2.127 

0.0 -6.381 

2.5 -.709 

2 .. 5 -2 .. 127 

2.5 -20.561 

2.5 -20.561 

3.0 -4.963 

2.5 19.852 

2.5 31.905 

2.5 31.905 

1.5 34.032 

3.5 2.127 

3 .. 5 2 .. 127 

1.0 -21 .. 979 

1.0 -21.979 

1.5 4.9b3 

1.5 4.963 

2.0 30.487 

2 .. 0 30.487 

2.0 42.540 

2.0 39 .. 704 

1.5 44.667 

1 .. 5 44.667 

1.5 -30 .. 487 

1..5 -30~4Bl 

1 .. 5 -39.704 

2 .. 0 4.254 

2.0 -29 .. 069 

2.0 -29.0b9 

2.0 34.032 

2 .. 0 34~032 

2.0 43.249 

A-13 
I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Ace. 

NO. 

REV 038 

SYSTEM 

TIME 

SoC 

1 12776.14 

12788.24 

12852.64 

4 12886 .. 84 

5 12900.94 

6 12920 .. 94 

7 12933.04 

8 12963.04 

9 12914 .. 34 

10 12994 .. 94 

11 13103.34 

12 13117.54 

13 13246.94 

14 13257 .. 44 

15 13281.24 

16 133215.34 

17 13356.14 

Ie. 13382.94 

19 13393.44 

20 13447.14 

21 13471.14 

22 13485 .. 24 

23 13497.04 

24 13507 .. 44 

25 13519.14 26 13817.(34 

27 13921.54 

28 13936.14 

29 13951.34 

RtV f)39 

1 18Q6-{ e 14 

2 18078.44 

18316.14 

18327.44 

18354 .. 84 

18537.54 

18548 .. 84 

18563.34 

9 18619.14 

10 IB630 .. 84 

11 18673.74 

U 1t:bR7.74 

13 1869!j.74 

14 18727.14 

]? 18742.94 

16 18752.94 

17 18852 .. 04 

18 18il63.7i t 

F F V 040 

23341 .. 24 

23356.14 

23450 .. 34 

23464 .. 44 

23419.24 

23494.14 

23675.94 

23739.24 

9 23755.34 

10 23804.84 

11 23817 .. 34 

U 23851.94 

13 23862 .. 44 

14 23886.44 

15 23898.14 

16 23911.64 

17 24032 .. 74 

BURS T 

T I '''''E 

SEC 

7 .0 

7.4 

5.1 

5.1 

5.1 

6.7 

6.7 

7.1 

7.1 

6.3 

7.6 

7.1 

12.5 

5.4 

.':>.3 

9.8 

6.3 

6.3 

8.6 

9.4 

5.3 

5.3 

6.3 

8.4 

5.0 

11.3 

10.6 

5.1 

5.9 

9.0 

7.1 

7.1 

5.3 

5.9 

5 .. 9 

5.8 

6.3 

6.3 

5.3 

6.0 ,.3 

5.3 

6.3 

6.3 

7.5 

7.,:; 

'>.9 

5.9 

6.8 

7.1 

5.9 

5.9 

5.0 

5.1 

6.6 

6.3 

9C?1 

DEG 

72 

71 

67 

64 

62 

59 

57 

50 

49 

40 

39 

38 

34 

32 

31 

26 

24 

24 

23 

22 

21 

1 

5 

6 

7 

74 

73 

57 

55 

42 

40 

37 

33 

32 

31 

29 

28 

27 

21 

70 

69 

68 

55 

51 

46 

43 

40 

40 

39 

30 

COM/olAND PO SIT rON 

LAT LONG 

MIN DEG 

08N 

20N 

06N 

49N 

42N 

33N 

12N 

14N 

24N 

4LN 

03N 

49N 

52N 

05N 

40N 

5aN 

o 3N 

14N 

31N 

43N 

ION 

57S 

57S 

595 

16N 

32N 

45N 

08N 

41N 

55N 

06N 

22N 

24N 

39N 

42N 

3 6~~ 

55N 

DoN 

23N 

25N 

29N 

31N 

19N 

DIN 

33N 

20N 

59N 

llN 

15N 

51N 

131 

130 

127 

125 

124 

122 

122 

119 

119 

116 

116 

116 

115 

115 

115 

114 

113 

113 

113 

113 

113 

110 

108 

108 

108 

112 

III 

99 

98 

95 

94 

94 

93 

93 

92 

92 

92 

92 

91 

95 

85 

84 

83 

76 

75 

74 

73 

72 

72 

72 

70 

MIN 

40E 

48E 

08E 

38E 

20E 

5SE 

03E 

31E 

14E 

59E 

49E 

28E 

47E 

23E 

02E 

l3E 

54E 

44E 

36E 

28E 

20E 

DOE 

52E 

43E 

33E 

13E 

13E 

S7E 

57E 

20E 

55E 

04E 

17E 

06E 

57E 

35E 

23E 

15E 

02E 

46E 

30E 

39E 

49E 

49E 

23E 

07E 

170 

44E 

33E 

20E 

38E 

CO"MIND INFOR"ATI0N 

BEST oPHEMERIS LAT LONG 

DEG MIN 

72 8.74N 

71 21.49N 

67 7.06N 

64 50.46N 

63 53.93N 

62 33.54N 

61 44.82N 

59 43.72N 

58 58.01N 

57 34~'57N 

50 13 .45N 

49 15.45N 

40 25.36N 

3g 42 .. 24N 

38 4 .. 45N 

34 50.14N 

32 53.83N 

31 5.92N 

30 22.66N 

26 41.29N 

24 59.83N 

24 4.14N 

23 15.,45N 

22 32. 54N 

2L 44.25N 

1 11.53N 

5 55.575 

6 55.635 

7 58.135 

14 16.37N 

73 32.91N 

57 45.90N 

57 .oaN 

55 8.80N 

42 42.39N 

41 56.03N 

40 56.52N 

37 7.26N 

36 19.14N 

33 22.60N 

32 24.96N 

31 39.65N 

29 42.64N 

28 37.52N 

27 56.29N 

21 7.48N 

20 19 .. 19N 

77 23.83N 

76 28.59N 

70 25.78N 

69 30.21N 

68 31.66N 

61 32.50N 

55 20.11N 

51 2.30N 

49 56.S8N 

46 34 .. Z0N 

45 43 .. 02N 

43 21.24N 

42 38.18N 

40 59.69N 

40 11.65N 

39 16.20N 

30 57.93N 

DEG MIN 

131 40.65E 

130 48 .. 89E 

127 8.21E 

125 37.87E 

125 4.52E 

124 20.49E 

123 55.51E 

122 58.23E 

122 38.17E 

122 3.49E 

119 31.32E 

119 14.2oE 

116 58.72E 

116 48.95E 

116 27.35E 

115 46.54E 

115 23.01E 

115 1.93E 

114 53.64E 

114 12.44E 

113 54.!7E 

113 44.2RE 

113 35.72E 

113 28.23E 

113 19.86E 

109 59.61E 

108 52.28E 

108 42. 75E 

L08 32.81E 

112 13.98E 

111 D.09E 

99 56 eSSE 

99 38.33E 

98 56.58E 

95 19.38E 

95 8.33E 

94 54.43E 

94 3.62E 

93 53.44E 

93 l7.32E 

93 5.90E 

92 57.05E 

92 34.63E 

92 22.42E 

92 14.77E 

91 2.13E 

9U 53 .. 87E 

95 47.21E 

93 4B.40E 

85 29.99E 

84 39.00E 

83 49.69E 

83 3.87E 

76 49.29E 

75 23.30E 

75 3 .. 47E 

74 6.66E 

73 53.18E 

73 17.43E 

73 7.00E 

72 43.80E 

72 32.80E 

72 20.33E 

70 37.62E 

Handle via Byeman 

Controls Only ~-GAMBIT 

Handle via Byeman 

Controls Only 

FILM VELOCITY IN./SEC. MIRROR CRAB ROLL 

COW-iAND 

2.8840 

2.9419 

2 .. 4841 

2.6899 

2.6633 

3.0614 

3.0311 

3.1229 

3.1857 

2.7168 

2.5089 

2.5594 

3.2497 

3.2822 

2 .. 7440 

2.9L28 

2.9419 

3.2497 

3.3482 

2.9128 

3.7728 

3.4155 

3 .. 62 56 

3.2497 

3 .. 2!;.l'Z 

3.3150 

2.5594 

2.5850 

2.7714 

3.1541 

3.1857 

3.1857 

3.1857 

3.6619 

3.1541 

3 .. 1229 

3.38LI 

3.1541 

3.0920 

3.0011 

2.8840 

3.1229 

2.B554 

3 .. 5 190 

3.848-' 

3.0311 

2 .. 9419 

2.4841 

2.41541 

2.5340 

2.5594 

2. 'tB41 

2.4841 

3.4841 

2 .. 4841 

2.4841 

2.8271 

2.9128 

3.3150 

3.2822 

3 .. 1851 

3.2175 

3.5897 

3.3150 

ACTUAL 

2.885 

2 .. 944 

2.485 

2.691 

2.662 

3.061 

3.031 

3.124 

3.189 

2.717 

2.510 

2.556 

3.248 

3.284 

2.743 

2.913 

2.940 

3.247 

3.347 

2.911 

3.775 

3.416 

3.623 

3.247 

3.284 

3.316 

2.554 

2.587 

2.770 

3.1 52 

3.\86 

3.187 

3.187 

3.660 

3.152 

3.122 

3.384 

3.150 

3.094 

3 .. 000 

2.882 

3.124 

2 .. 852 

3.521 

3.846 

3.032 

2.939 

2.4B9 

2 .. 't89 

2.533 

2.563 

2.489 

2.489 

3.489 

2 .. 489 

2.489 

2 .. 827 

2.911 

3.315 

3.28 4 

3.189 

3.218 

3 .. 591 

3.313 

POS. DEG. ANGLE 

.5 -?4.815 

1.0 -25.524 

.5 -41.122 

1.5 33 .. 323 

1.5 33.323 

2.0 21.270 

2.0 21.270 

1.5 -22.6B8 

1 .. 5 -22.688 

1.5 -38~286 

laO -43.958 

2 .. 0 -43 .. 958 

2.5 -24.106 

2.5 -24 .. 106 

2~O -44.667 

2 .. 0 -41. 122 

2.0 -41.1?2 

2.5 -2I t.815 

2.5 -?4.B15 

2.5 -41.R31 

3 .. 0 -11.344 

3.0 -17.016 

3 .. 0 -20.561 

3.0 -24.El15 

3 .. 0 -24 .. 815 

3.0 17.725 

3.0 -38.286 

3.5 -"18.995 

3.5 -31.905 

l.O -6.381 

1.0 -6 .. 381 

2.0 17.725 

2.0 17.725 

2.0 2.836 

2~5 24.106 

2.5 24.106 

2.5 16.307 

2.5 26.942 

2.5 ;6.942 

2.0 -41.831 

2.0 -43.958 

2 .. 5 -3R~99, 

2.0 -44.(J67 

3 .. 0 -17.(116 

3.0 -14.180 

3 .. 0 27a651 

3aO -n .. 651 

0 .. 0 -'IR.99S 

0.0 -38.995 

1.5 36.159 

1.0 16.H6d 

1.5 3fl. <195 

1.5 38.995 

2.0 -19.143 

2 .. 0 45.376 

2 .. 0 45 .. 376 

1.5 -36.868 

1.5 -36 .. .868 

2.5 17 .. 725 

2.5 17 .. l25 

2 .. 0 -26.942 

2 .. 5 -26.942 

2 .. 5 -2:) .. 524 

2.5 26.'.J't2 

Approved for Release: 2018/09/11 C051 03025 

A-14 
I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

rrApproved for Release: 

~ 

2018/09/11 C051 03025 ~.L U..L.J'-'.J..\..A...J..L '-A.J.-1l..J.V.1.,LJ .... .&. 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

COMMAND INFORMATION 

Handle via Byeman 

Controls Only 

Ace .. BURS T 

Tj ME 

COMMAND pos IT ION 

LAT LONG 

BE:ST E:PHEMERI S FILM VELOC ITY I N .. /SEC. MIRROR 

CRAB ROLL 

NO. 

SEC 

RE: v 041 

1 28621.74 

2 28634 .. 64 

3 28667~24 

2861:11.14 

28695.24 

28749.24 

28762.54 

28788.14 

9 28817 .. 84 

10 28929.04 

11 28939.54 

12 28Y54.04 

13 28964.54 

14 28992.74 

15 29010.74 

16 29024.84 

17 2903') .04 

18 29052.34 

19 29097.64 

2029108.14 

21 29123.04 

22 29171.54 23 29182.84 

24 29210.74 

25 29221.64 

26 29236.94 

27 29247 .. 54 

28 2933:) .04 

29 29354 .. 44 

30 29365.24 

31 29439.14 

32 294?O~04 

33 Z9')g8.R4 

34 29613.34 

35 2964S.84 

36 29656.34 

37 29803.24 

38 29814.94 

39 29986.44 

40 29999 .. 74 

41 30016.84 

42 30028.54 

REV D42 

1 33923 .. '14 

2 33937 .. 24 

3ft 12 3.64 

3i~ 134 .. 94 

341&7 .. 44 

6 34182.74 

7 34214.94 

e 34224 .. ~lt 

9 3't239 .. 04 

10 34252.34 

11 34278.74 

12 34289 .. 6 4 

13 34301 .. 54 

14 34324.04 

15 34340 .. 54 

16 34359.24 

17 34370 .. 14 

18 34385.54 

19 34':396.04 

20 34/+06 .. 54 

21 34428.34 

22 344:'2 .. 44 

23 34462.94 

24 34474.74 

25 34500.54 

26 34511 .. 84 

27 34:;22.24 

28 34554 .. 24 

29 34564.34 

30 34700 .. 04 

31 34710 .. 14 

32 34845.44 

33 34855 .. 54 

34 34990 .. 64 

3' 35001.54 

36 3')086.34 

37 3:'100.84 

38 3~130.64 

39 35219.94 

LIO 35;~'S9.94 

itl 3')273.114 

42 352g0 .. 84 

4-) 35jQ4 .. 14 

44 3'j1~'J .. 2/. 

45 15 j<)O .. 1 I. 

46 3 c,) to. I.i. 

47 3'):'20 .. 94 

Handle via Byeman 

Controls Only 

SEC 

0.1 

5.1 

5.1 

~.1 

5.1 

5 .. ? 

5.5 

5.5 

5.6 

6.9 

6.9 

6.0 

7.1 

9.7 

5.1 

5.1 

6.7 

6.9 

6.3 

6.3 

5.3 

7.1 

7.1 

5.5 

5.5 

5.4 

9.0 

5.3 

7.3 

7.8 

7a9 

7.9 

6.7 

6.7 

6.3 

6.2 

6.3 

6.2 

').5 

5.5 

7.1 

7.1 

5.5 

5.5 

5.9 

:' .. '1 

5.'1 

').9 

5. 9 

5.9 

5.9 

5.5 

0.5 

5 .. 5 

~. :} 

DEG 

79 

77 

76 

72 

69 

67 

60 

59 

58 

57 

55 

54 

52 

51 

48 

46 

43 

40 

39 

38 

32 

31 

30 

25 

14 

11 

10 

o 

o 

12 

14 

15 

81 

68 

65 

64 

62 

6< 

61 

58 

57 

56 

55 

54 

52 

:)2 

51 

50 

49 

48 

46 

45 

45 

43 

41 

39 

29 

19 

3 

2 

o 

1" 

14 

MIN DEG 

59N 

17N 

25N 

05N 

32N 

34N 

06N 

25N 

27N 

44N 

50N 

37N 

4HJ 

47N 

42N 

58N 

40N 

59N 

llN 

28N 

28N 

08N 

23N 

1 BN 

19N 

05N 

22N 

16N 

325 

175 

22S 

105 

ION 

44N 

50N 

49N 

40N 

01N 

DiN 

22N 

38N 

49N 

18N 

llN 

55N 

10N 

08N 

25N 

42N 

13N 

34N 

51N 

03N 

17N 

48~~ 

37N 

37N 

37N 

38N 

03N 

03N 

OON 

075 

52S 

595 

OiS 

81 

73 

71 

65 

62 

60 

56 

56 

55 

55 

54 

54 

53 

53 

52 

52 

51 

50 

50 

49 

48 

48 

48 

47 

45 

45 

44 

43 

43 

41 

40 

40 

64 

39 

37 

36 

35 

35 

34 

33 

33 

33 

32 

32 

31 

31 

31 

30 

30 

30 

29 

29 

29 

28 

28 

28 

25 

24 

22 

21 

21 

21 

20 

19 

19 

1 B 

16 

MIN 

220 

2IE 

31E 

D2E 

30f 

54E 

35E 

16E 

5lE 

33E 

49E 

23E 

43E 

26E 

31E 

02E 

llE 

32E 

08E 

5SE 

44E 

28E 

20E 

23E 

31E 

OOE 

53E 

17E 

09E 

17E 

57E 

49E 

3IE 

38E 

30E 

52E 

38E 

18E 

49E 

37E 

19E 

ODE 

26E 

02E 

37E 

2?E 

02E 

49E 

37E 

llE 

44£ 

33£ 

20E 

54f 

32E 

02E 

59E 

13E 

34E 

32£ 

22E 

03E 

05E 

39E 

18E 

49E 

LAT LONG 

OEG fUN 

79 57.85N 

79 13.15N 

77 15.57N 

76 23.93N 

75 30.88N 

72 3.11N 

71 1l .. 12N 

69 30.40N 

67 32.68N 

60 6.44N 

59 23.99N 

58 25.29N 

57 42.74N 

55 48.29N 

54 35~12N 

53 37.73N 

52 39.89N 

51 45 .. 67N 

48 40.72N 

47 57.79N 

46 56.83N 

43 38.17N 

42 51.83N 

40 57 .. 34~~ 

40 12.59N 

39 9.74N 

38 26.18N 

32 26.19N 

31 6.28N 

30 21.78N 

25 17.10N 

24 32.14N 

14 18 .. 00N 

13 18.!4N 

11 3.98N 

10 20.65N 

o 14.74N 

o 33.475 

12 18.795 

13 13 .365 

14 23.4gS 

15 11~45S 

81 9.46N 

80 26 .. 0m~ 

68 44.26N 

67 59.44N 

65 49.94N 

64 48.72N 

62 39.4lN 

62 .. 75N 

61 2.28N 

60 8.~7N 

58 21.76N 

57 37.58N 

56 49.31N 

55 17.9 2N 

54 10.SlN 

52 54.66N 

52 10.24N 

51 7.43N 

50 24 .. 57N 

49 41.69N 

48 12.60N 

46 34.00N 

45 51aU2N 

45 2.68N 

43 16.93N 

42 30.58N 

41 47.91N 

39 36.52N 

38 55.03N 

29 36.52N 

28 54.89N 

19 36.75N 

18 55.06N 

9 37.39N 

8 52.41N 

3 2 ~ 6UN 

2 2.82N 

o O. OON 

7.65 S 

52 .. 105 

48 .. 395 

10 59.02S 

11 53.625 

14 1. 215 

15 2.3U5 

25 57 .. 495 

?7 4.71S 

DEG MIN 

81 16. 17E 

78 37.05E 

73 17.20E 

71 28.07E 

69 50.03E 

65 .04E 

64 3.89E 

62 27.95£ 

60 52.77E 

56 34.34E 

56 15.31E 

55 50.13E 

55 32.63E 

54 48.34E 

54 21.9lE 

54 2')lE 

53 42.89E 

53 25.49£ 

52 30.15E 

52 18.09E 

52 1.41 E 

51 10.26E 

50 58.96E 

50 31.92E 

50 21.67£ 

50 7.56E 

49 57.96E 

48 43.42E 

48 27.81£ 

48 19.34E 

47 23.12E 

47 15.10E 

45 30.88E 

45 21.12£ 

44 59.41£ 

44 52 .. 45E 

43 16.49E 

43 8.91E 

41 16.72E 

41 7.85E 

40 56.39E 

40 48.50(: 

64 29.28E 

61 .82E 

39 37.50E 

39 1.8lE 

37 29.92E 

36 51.36E 

35 38.11E 

35 18.08E 

34 49.18E 

34 23.99E 

33 37.33E 

33 19.21E 

33 .13E 

32 25.85£ 

32 2.07E 

31 36.37£ 

31 21.94E 

31 2.20£ 

30 49.14E 

30 36.39E 

30 10.84E 

29 43.90£ 

29 32.55E 

29 20.06E 

28 53.65E 

28 42.45E 

28 32.3lE 

28 2ol2E 

27 52.89E 

25 59.32E 

25 51.49E 

24 12.45E 

24 5.40E 

22 34.05E 

22 26.86E: 

21 31.43E 

21 22.02E 

21 2.69E 

20 4.68E 

19 38.49E 

19 29.48E 

19 18. 12E 

19 9.30E: 

HI 4H.53E 

IH "38.50E 

16 4S.85E 

16 33 .. 60E 

T~-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

COMMAND 

2.9128 

2.941 9 

2.5594 

2.6899 

2.7168 

2.8271 

2.8271 

3.1541 

2.4841 

3. 31 ~o 

3&3150 

3.3482 

3 .. 3482 

2.9419 

2 .. 7440 

2.7168 

2.8271 

2 .. 7991 

3.3150 

3.3150 

3.4841 

3.2175 

3.1857 

3.4841 

3.4841 

3 .. 2175 

3.0011 

2.6108 

3.3150 

3.3482 

3 .. 3482 

3.3150 

2 .. 5340 

2 .. 5850 

3.4155 

3.3817 

2.9713 

3.0011 

2.7991 

2.8271 

3.0011 

3.G!) 11 

2.8271 

7 .. 1:1 ')54 

3 .. 2497 

; .. ')497 

2.5089 

2.5089 

3.1541 

3.31:117 

2.7714 

2.8??1 

3 .. 3482 

3.3817 

3.5542 

2.7991 

2.8271 

3.3150 

3.3482 

3.4496 

3.4496 

3 .. 4496 

3.4496 

3 .. 41:141 

3.4841 

3.5897 

3 .. 1541 

3.1857 

3.0011 

3 .. 5542 

3 .. 5542 

3 .. 554? 

3 .. 5::>42 

3 ~ 5 190 

3 .. 4841 

3.4155 

3.3817 

2.6633 

2 .. :'850 

3.4H41 

3 .. 0614 

2.7714 

2 .. 6S 0 9 

2 .. 8840 

2.11271 

2. ')OH9 

:' .. 4841 

2 .. 4d41 

2 .. 4K41 

AC TUAL 

2.913 

2 .. 940 

2.559 

2.695 

2.716 

2.826 

2.826 

3.155 

2.488 

3 .. 316 

3 .. 316 

3.345 

3.345 

2.945 

2 .. 743 

2.715 

2 .. 826 

2.800 

3.314 

3.314 

3.486 

3.217 

3.187 

3.486 

3.486 

3.219 

3.000 

2.638 

3.312 

3 .. 34'1 

3.349 

3.315 

2 .. 533 

2.591 

3.417 

3.382 

2 .. 969 

3.000 

2.800 

2.827 

3.000 

3.000 

2.825 

2 .. 849 

3.247 

3.247 

2.509 

2.509 

3.150 

3.380 

2.769 

2.823 

3.345 

3.381 

3 .. 553 

2.800 

2.822 

3.314 

3.347 

3.447 

3.447 

3 .. 446 

3.448 

3.487 

3.487 

3.593 

"3 .. 153 

3.184 

3.000 

3.551 

3.553 

3 .. 553 

3.553 

3.518 

3.489 

3.416 

3.382 

2.659 

2.584 

3.487 

3.058 

2.769 

2 .. 691 

2.883 

2 .. 827 

2 .. 509 

2.484 

2.485 

2.487 

POS .. OEG. ANGL F 

.5 -19.143 

.5 -19.143 

0.0 -34.032 

.. 5 -:11 .. 196 

.5 -31.196 

1 .. 5 26 .. 942 

1.5 26.942 

1.0 -12.762 

1 .. 0 38.99') 

2~O 7 .. 090 

2.0 7.090 

2.0 7.799 

2 .. 0 7 .. 799 

2.0 28.360 

2.0 34.741 

2.0 34 .. 741 

2 .. 0 32.h14 

2.0 32.6lt~ 

2.5 14.HElY 

2 .. 5 14 .. 8£19 

2.5 -6.381 

2.5 21.270 

2.5 21.270 

2.5 -12.053 

2.5 -12.053 

2.5 -27.'51 

2.5 -34.741 

2.0 -43.249 

2 .. 5 -25.5;:4 

3.0 -75.524 

3.0 -21.270 

3.0 -24.10tJ 

2.5 -44.667 

2.5 -44.667 

3.5 2.806 

3.5 2.836 

3 .. 5 -26.942 

3.5 -26.942 

3.0 -25 .. 52'~ 

3 .. 0 -25.')24 

3 .. 5 -7..7YQ 

3.5 -7.799 

0 .. 0 -.U.68B 

0 .. 0 -22 .. fdlK 

1.5 4. 2<,"!-

1 .. 5 4.2~4 

1 .. 5 38.99') 

1.5 38.9Y5 

1 .. 5 -20 .. ~)61 

1.5 -20.561 

1.0 -34.0.:32 

1.0 -34 .. 032 

2 .. 0 -9.g26 

2 .. 0 -4.926 

2 .. 0 -l{~aRi-lg 

1 .. 5 -41.122 

2 .. 0 -35 .. 4~0 

2 .. 0 -15.'5gf\ 

2 .. 0 -15.")98 

2.0 -6.381 

2.0 - 7.799 

2.0 -7 .. 799 

2.0 19.852 

2 .. 5 -8 .. 508 

2 .. 5 -8 .. 508 

2 .. 5 -19.B52 

2.0 -26.942 

2.0 -26.94? 

2.5 -34.032 

3 .. 0 -4~2S4 

3.0 -4.254 

3.0 -1 .. 545 

3 .. 0 -3.545 

3.5 -4.254 

3 .. 5 -4 .. 254 

3.5 -4.?54 

3.5 -4.?54 

3.0 34.032 

3.0 34.032 

3 .. 5 -9.?1? 

3.0 22.688 

3.0 25. 1:;24 

3.0 25 .. 524 

3 .. 0 19.143 

3.0 19 .. 14;1 

3.0 31.196 

3.0 31.196 

2.5 -39.704 

2.5 -39.704 

A-15 
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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

ACC. 

NO. 

REV 043 

SYSH:M 

T Itlf 

,EC 

BURS T 

T I !'\F. 

SEC 

1 39233.33 ':>.9 

39247 .. D3 5.9 

39407.63 5.3 

39438.43 5~9 

39'+/+9.73 5.9 

39461.93 5.6 

39488 .. 73 5 .. 5 

8 39502.03 5.5 

9 39520.13 5 .. 9 

10 39531.43 5.9 

11 39574.13 5.5 

12 39587.43 5.5 

13 39622.53 6.3 

14 39636.63 6.3 

lS 39647.[1'3 10.3 

16 39664.73 16 .. 7 

17 39685.13 5.5 

18 39699.63 6.5 

19 39714.33 6.1 

20 39818.83 7.1 

21 39828.93 7.1 

22 39903.13 8.3 

23 39915.63 8.3 

24 39959.93 6.3 

2~ 39974.03 6.3 

26 40009.23 5.3 

27 '10121.13 5.5 

28 40135.63 5.5 

29 40244 .. 83 7.5 

30 40257.73 7.5 

31 40343.33 6.3 

3;:' 4035::>.03 6.3 

33 4036tl.B3 5.6 

REV D44 

1 

2 

REV D47 

1 

2 

3 

10 

!l 

12 

13 

14 

15 

Ri-V U48 

44595 .. 43 7.1 

44609.13 17.4 

'+4856.23 683 

44869.13 6.3 

45291.63 6.3 

45303.33 7.0 

60597.73 :::.9 

60609 .. 03 5.9 

60838.03 ':>~5 

f.0!348 .. 93 ".'; 

b1020.23 3.9 

61030 .. 73 3.9 

61118 .. 63 100.1 

6122l .. 93 h.3 

612')1.23 7~1 

6126Y.43 7.3 

61280.33 7.7 

61595.33 3.9 

61607.03 3.9 

617'+8 .. 73 5.1 

61760.43 5 .. 1 

1 66131 .. 63 2(-t.8 ".5 

5.5 

6.3 

6.3 

6.3 

8.2 

5.9 

5.9 

5.1 

7.1 

7.0 

2 66187.'t3 

66198 .. 33 

66330.63 

66343.53 

66407.43 

66 4 17.53 

66460.93 

66471..03 

to 6648U.53 

11 66489.13 

12 66602 .. 23 

Rt'"V D49 

1 72710.22 

2 72723.92 

ReV flSU 

1 7&697.62-

2. 76709.32 

3 76817 .. 62 

76828 .. 52 

7.1 

7.1 

COM,~lANLJ pus I T ION 

LA T LONG 

DEG r'll N OEG 

81 54N 

71 2lN 

69 20N 

67 47N 

66 OON 

63 54N 

60 17N 

57 olN 

55 18N 

54 09N 

52 46N 

51 47N 

50 47N 

43 40N 

37 54N 

34 OON 

30 37N 

22 55N 

] '+ 25N 

79 

79 

63 

33 

32 

62 

50 

43 

35 

34 

32 

32 

10 

64 

60 

50 

45 

44 

41 

40 

40 

32 

21 

69 

61 

38N 

53N 

51N 

03N 

06N 

28N 

40N 

59N 

20N 

01N 

18N 

'J9N 

13N 

58N 

13N 

34N 

01N 

19N 

34N 

52N 

38N 

57N 

59N 

38N 

o3N 

18N 

335 

34N 

34N 

46 

19 

17 

16 

15 

12 

10 

10 

9 

9 

9 

14 

11 

8 

17 

17 

58 

75 

80 

82 

83 

84 

84 

84 

88 

89 

96 

98 

102 

103 

103 

104 

10" 

105 

106 

137 

137 

142 

46E 

52E 

57E 

41E 

25E 

08E 

17E 

53E 

15E 

50E 

22E 

03E 

45E 

48E 

28E 

39c 

59E 

35E 

09E 

04E 

13W 

17E 

32 E 

31W 

39W 

48. 

07" 

29W 

15W 

03W 

44W 

04W 

19W 

28W 

14W 

54" 

35W 

33" 

l1W 

39W 

50W 

33W 

52" 

OOW 

38W 

47. 

llW 

26" 

COM~ANO INFORMATION 

BEST EPHEI>lERI S 

LAT LONG 

DEG MIN 

81 54.60N 

81 12.30N 

71 21.80N 

69 20.63N 

68 35.91N 

67 47 .. 49N 

66 .69N 

65 7.50N 

63 54.93N 

63 9.54N 

60 17.42N 

59 23.b5N 

57 1.43N 

56 4.19N 

55 18.68N 

54 9.94N 

52 46.86N 

51 47.·15N 

50 47.78N 

43 40.23N 

42 58 .. 82N 

37 54.12N 

37 2.73N 

34 .47N 

33 2.42N 

30 37.43N 

22 55.99N 

21 56.16N 

14 25.42N 

13 32.17N 

79 

79 

63 

62 

33 

32 

77 

77 

62 

61 

50 

49 

43 

35 

34 

32 

32 

10 

9 

o 

o 

64 

60 

59 

50 

49 

45 

44 

41 

41 

40 

40 

32 

38.88N 

50.61N 

53.68N 

51.54N 

3 .. 8'tN 

6.38N 

14.46N 

2f3.77N 

40.59N 

58.89N 

17.51N 

20.57N 

3G .. 64N 

.84N 

17.9SN 

18.08N 

49.08N 

13 .20N 

58.27N 

13.39N 

33.93N 

45.65N 

1.33N 

46.865 

18.93N 

34.25N 

50.! 9N 

52o.'t5N 

59.78N 

38.41N 

57.03N 

59.07N 

!7 .61N 

3B .. 61N 

3.29N 

18.09N 

21 34.295 

22 30.225 

69 3i,..23N 

68 47.9 Ld\l 

61 31+.5 2N 

60 5U.53N 

OEG MIN 

46 47.83E 

42 33.46E 

19 52.50E 

17 56.8'-tE 

17 19.3lE 

16 41.29E 

15 25.6lE 

14 51.5lE 

14 8.24E 

13 42.88E 

12 16 .. 63E 

11 52.42E 

10 53.42E 

[0 31.48E 

10 14.69E 

9 50.33E 

9 22.35E 

9 3.33E 

8 44.72E 

6 47 .. 90E 

6 37.78E 

5 28.09E 

5 17.05E 

4 39.29E 

4 27.,67E 

3 59.4lE 

2 35.24E 

2 24.83E 

1 9.13E 

1 .44E 

o 3. 64E 

o 4.03. 

o 13.05W 

14 

11 

8 

8 

17 

17 

58 

59 

75 

75 

80 

80 

82 

83 

84 

84 

84 

88 

88 

89 

90 

96 

98 

98 

102 

102 

103 

103 

104 

104 

104 

105 

106 

18.71E 

33.59E 

30.31. 

5"1.79W 

38.55W 

48.12W 

7.57. 

'+7.61W 

29.24" 

51.52W 

15 .. 26\00/ 

27 .83" 

3.30W 

44.16W 

3.82. 

18.83" 

2"I.68W 

13.93" 

21..67W 

54. lOW 

1.68" 

35.21W 

32.82W 

53.03W 

10.96. 

26.82. 

39.24W 

49 .. 88W 

33.54W 

43o.26W 

52.27101 

.31" 

38.02W 

137 47.01W 

137 56 .. 73101 

137 10.45W 

137 50.02W 

142 25.63w 

142 '+6 .. 98w 

Handle via Byeman 

Controls Only ~-GAMBIT 

Handle via Byeman 

Controls Only 

FILM VELOCITY IN./SEC. MIRROR 

CRAB ROLL 

COMMAND 

2.6899 

2.7168 

2.5340 

3.1541 

3.1857 

2.9128 

2.8271 

2.7991 

3.2175 

3.2175 

2.8271 

2.8840 

2.6369 

2.6108 

2.5340 

2.5089 

2 .. 5594 

2.5340 

2~5594 

3.4841 

3.5190 

2.8271 

2 .. 8 840 

2.6108 

2.5594 

3.0920 

2.5594 

2.6108 

2.7991 

2. ·1440 

3.0920 

3.03!! 

3.5542 

2.6108 

2.6369 

2.7440 

2.7't40 

3.0614 

3.0011 

3.1229 

3.1541 

3.3482 

3.3482 

3.4496 

3.4841 

3. n28 

3.3817 

3.8106 

3.3150 

3.3482 

3.3817 

3 .. 3817 

3.2497 

3.2497 

3.3817 

3.3482 

3.3817 

2.7440 

2.7).68 

3. '+841 

3.484 1 

3.5542 

3.5897 

3 .. 5542 

3.8106 

3.H871 

2.5850 

2.6369 

3.249 I 

3.2H2c' 

3.34R? 

3.3817 

ACTUAL 

2 .. 693 

2.719 

2.536 

3.153 

3.189 

2.916 

2.825 

2.796 

3.217 

3.217 

2.829 

2.888 

2.634 

2.611 

2.534 

2.508 

2.560 

2.530 

2.556 

3.484 

3.518 

2.824 

2.886 

2.608 

2.556 

3.093 

2.555 

2.607 

2.799 

2. "140 

3.089 

3.029 

3.550 

2.610 

2 .. 636 

2 .. 740 

2.740 

3.059 

2.997 

3.122 

3.150 

3.346 

3.346 

3.449 

3 .. 483 

3.768 

3.384 

3.808 

3.312 

3.347 

3.382 

3.382 

3.244 

3.249 

3o.38't 

3.344 

3.380 

2.740 

2.714 

3.487 

3. 4 84 

3.550 

3.591 

3.551 

3.809 

3.889 

2.587 

2.634 

.249 

.286 

.344 

.385 

P05. OEG. ANGLE 

1.0 26.942 

1.0 26.942 

1.0 41.122 

1.0 -13.'+71 

1.0 -13. ft71 

1.0 -26.942 

1.5 29.778 

1.5 2q.778 

1.5 13.40 

1.5 13.471 

1.0 -32.614 

1.0 -32.614 

2.0 36.868 

2 .. 0 36 .. 868 

2.0 42.')40 

2.0 42.540 

2.0 39 .. 704 

2.0 394704 

1.5 39.704 

2 .. 5 -8.508 

2.5 -8.508 

2 .. 5 34.741 

2.'5 31. Q 05 

2.5 40.413 

2 e:;' '+0 .. LJ 13 

3.0 -33.323 

2.0 -43.958 

2.0 -43.951:1 

3 .. 0 33.323 

3.0 3~.:~23 

3.0 21.270 

3.0 21.270 

3.5 6.381 

1.0 

1.0 

1.5 

1.5 

2.5 

2.5 

.5 

.5 

1.5 

1.5 

2.5 

2.5 

2.5 

3.0 

3.0 

3.0 

3.0 

3.5 

3.5 

3.5 

31.! 96 

31.! 96 

32.614 

32 .. 61'+ 

28.360 

2R.360 

-78 ago -7.000 

-4 .. q63 

-It 0 OA·~ 

-7.799 

-7.799 

-.709 

-20 .. 561 

-5.672 

-22.688 

-22.688 

-9.217 

-9. ~ 17 

-9. 2! 7 

-9.217 

0.0 -6.381 

1.') -7.090 

1.5 -7.090 

2.0 35.450 

2 .. 0 35 .. 450 

2.5 7.799 

2.5 7.799 

2.5 -1.418 

2.5 -1.418 

;:'.5 1.418 

2.5 3.545 

3.0 .709 

3.0 -26.942 

3 .. 0 -26.942 

1.0 -6.381 

1.0 -6 .. 381 

1.5 -7 .. 090 

1 .. 5 -7 .. 090 

A-16 

Approved for Release: 2018/09/11 C051 03025 
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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Ace. 

NO. 

ReV 052 

REV D53 

SYSTEM 

T I rolE 

5EC 

909 .. 32 

921.02 

944 .. 32 

1000.02 

101 't.12 

1031.02 

)046.72 

1 6285.72 

2 6296.22 

3 6389.02 

4 6400.72 

) 6'+L::~02 

6 6632.32 

7 6642.82 

B 7~90.12 

9 7302.62 

10 7462.62 

11 747't.32 

12 7~94.32 

13 7D06.82 

14 7720.32 

15 7740 .. 02 

Rf V nS't 

1 11 ') 10 .. 92 

2 11532.22 

11552.02 

llb6~~32 

11076.42 

11692.32 

117()4 1O D2 

1171 g .. 02 

11740.82 

10 1175').32 

il 11875.32 

12 1188L42 

13 1191,2.12 

14 11929.72 

15 11940.22 

16 11964.72 

17 11983.02 

HI 11994.72 

19 12U06.92 

20 12028 .. ')2 

21 120-"'I:I .. h2 

~L 1,?u::;3 .. 92 

23 12070.22 

24 12081.52 

L~109.D2 

26 12134.72 

27 12141:1 .. '+2 

2H 121h.!.62 

29 ]2202 .. 12 

30 12220.42 

31 ]2237.82 

3? 12539.12 

33 1.?,)it 9 .. 62 

34 125Y:: .. 32 

3? U60Y.U2 

36 126~3.92 

37 12042.12 

38 12653.42 

39 12':,99.62 

(to 1?713.32 

R V D55 

1 16837.02 

16B53~':>2 

17126.12 

1 n~)U.82 

1716~.92 

17314 .. t!2 

1752?72 

173{~O.02 

173?8.12 

1U 1737'+032 

1117389.22 

12 17445 ... 42 

1.-; 174()9 .. ~2 

14 ]7482472 

1~; 17{t4B~7,? 

1 b 1 "1'>14 .. U2 

17 1-'':>4~~62. 

1 R 1 7::;':ob. I? 

19 17:''10.42 

;0 17006.:>2 

.::1 1706B.g2 

2.1 I/bliL02 

BURS T 

TIME 

SEC 

b.3 

0.3 

" .1 

5 .. 1 

':i.0 

6.3 

6.3 

7.1 

7.) 

6.3 

6.3 

5.9 

5.9 

:>.'1 

5.9 

5.5 

5 .. 5 

Sol 

Sol 

5. I 

7.5 

7. S 

I) .. 3 

9.0 

9.0 

5.5 

5.1 

S.l 

6.3 

6.7 

'.3 

COi·11-1ANO POSITION 

LAT LONG 

OEG MIN OEG 

71 'tUN 

69 22N 

65 40N 

63 36N 

68 03N 

61 09N 

5g 36N 

44 38N 

325 

12 2lS 

21 205 

3U 17S 

73 

71 

64 

62 

60 

59 

58 

49 

47 

'.6 

45 

43 

42 

41 

4() 

39 

37 

36 

35 

33 

32 

3i 

::;0 

27 

26 

25 

6 

7 

74 

5'. 

53 

52 

41 

41 

40 

36 

37 

32 

31 

30 

29 

28 

26 

(-t8N 

39N 

21N 

21N 

31N 

05N 

06N 

58N 

27N 

15N 

32N 

:,2N 

37N 

f t 9N 

59N 

30N 

't ~ ~~ 

38N 

52N 

?9N 

13N 

17N 

18N 

35N 

20N 

08N 

25N 

34N 

245 

395 

365 

325 

02N 

47N 

06N 

17N 

55N 

LON 

12N 

S 7N 

')lr-J 

,6N 

19N 

2,N 

i9N 

16[" 

n:;N 

ibN 

3 l r~ 

4 'IiI 

179 

178 

175 

174 

1 ?5 

150 

150 

145 

136 

135 

133 

i31 

138 

136 

130 

129 

128 

127 

127 

124 

123 

123 

123 

122 

122 

122 

122 

121 

121 

121 

121 

120 

120 

120 

119 

119 

119 

li8 

115 

)]4 

114 

ll4 

113 

il3 

116 

103 

103 

102 

100 

99 

99 

99 

99 

96 

97 

97 

97 

97 

96 

9, 

9') 

MIN 

30W 

170 

31 E 

PE 

02E 

49E 

06E 

liE 

SSE 

02E 

32 E 

SSE 

46E 

08E 

21E 

1SE 

20E 

42E 

HE 

27E 

45E 

25E 

14E 

49E 

30E 

19E 

on 

47E 

2 f tE 

10E 

ODE 

37E 

16E 

05E 

54t 

23E 

09E 

56E 

31E 

54E 

36E 

24E 

47E 

38E 

54E 

50E 

16E 

59t 

091:: 

59E: 

4bE 

29E 

14E 

14E 

54E 

4' .. E 

3H 

20e 

56E 

19i::: 

LBt 

19l: 

COMMAND INFORMATION 

BEST EPHEMERIS 

LAT LONG 

DEG MIN 

71 40 .. 28N 

70 54.44N 

69 22 .63N 

65 41 .. 02N 

64 1..4.56N 

63 36.72N 

62 33.?6N 

68 3.89N 

67 22.13N 

61 9 .. 82N 

60 22.57N 

59 36.87N 

44 3B.B9N 

43 5?85N 

o 31.425 

1 22.905 

12 20 .. 54$ 

13 8.525 

21 19.61 S 

22 10.645 

30 17.,265 

31 12.895 

73 49.28N 

72 ~7 .. 86N 

71 4U.7SN 

64 22.95N 

63 26.31N 

62 22.32N 

61 35.16N 

60 32.18N 

59 6 .. 43N 

58 7.69N 

49 59 .. 21N 

49 9.77N 

47 28.76N 

46 16.72N 

45 33 .. 71N 

43 53.30N 

42 38.25N 

41 50.24N 

41 .16N 

39 31.44N 

38 49.94tlj 

37 47.Ubti 

36 40.03N 

35 53.55N 

3 f t .. 39N 

32 1' •• S7N 

31 18. 14N 

30 19 .. 64N 

27 36.84N 

26 21.38N 

25 9 .. 63N 

4 26 .. 52N 

3 43.23N 

o 34.91N 

o 21 .. 515 

1 22.675 

2 37.795 

3 24.295 

6 34 .. 315 

7 30.025 

74 2.56N 

7258eR3N 

54 47.b1N 

~3 7 .. 04N 

52 17.711'" 

( .. 1 56. lIN 

'+ 1 11 .. 37i>J 

40 12 .. 6SN 

3B 51).29N 

37 51.7UN 

Jb 50 ~44N 

37 59.}7N 

31 19.9 IN 

30 2:·.53N 

29 19.60N 

2H Ib.':J4N 

26 6.25N 

2':> 22 eq');~ 

22 36 .. 71N 

21 5') .US,'" 

17 37 .. J)t'j 

16 47.621~ 

DEG MIN 

179 28 .. 94101 

179 43.19E 

178 17.43E 

i75 31.65E 

174 56.}6E 

174 16.86E 

173 42.57E 

155 1.7sE 

154 30.27E 

ISO 49.42E 

150 27.05E 

15{) 6.31E 

145 10.72E 

144 59.94E 

136 54. ?5E 

136 46.45E 

135 1.76E 

134 53 .. 96f: 

133 31.79E 

133 22.95E 

131 54.39E 

131 43.6n 

138 47.14E 

137 39 .. 49E 

136 9.63E 

)30 21.63E 

129 49.23E 

129 l' ... 90E 

128 50.97E 

128 20.67E 

127 42.IOE 

127 17.27E 

]24 27.'.2E 

124 12.96E 

123 44.58E 

123 25.2010 

123 13. 94E 

122 4B.50F. 

i22 3D.19E 

122 18.77E 

i22 7.08E 

12] 46.9H 

121 37.69E 

121 23.97E 

121 9.65E 

12u 59.90E 

120 36.7]E 

LW 15.67E 

12U 4.69E 

119 53.46E 

119 23.00E 

119 9.23E 

118 56.32E 

115 30.72E 

115 23.89E 

114 54 .. 24E 

114 4S.37E 

i14 35.71E 

114 23891E 

114 16.58E 

113 46.53E 

113 37.5BE 

116 54.74E 

115 29.hRF 

103 49.93E 

103 15.43E 

102 59032E 

IUU 9.33E 

99 5fi.ASE 

':19 4~o37E: 

99 2H.71E 

99 14 .. 15E 

99 1.04E 

98 1'.65E 

97 ')4.22E 

<..;7 43. 7eE 

')7 31.3UE 

47 19.53E 

g6 ?5.70E: 

96 it7~91E 

96 IB.5"/E 

'-i611.34E 

Y5 27.62E 

CIS 19.30E 

Handle via Byeman 

Controls Only J:OfJ SECREJ - GAMBIT 

Handle via Byeman 

Controls Only 

FILM VELOCITY IN./SEC. CRAB ROLL 

CDMt-1AND 

3.2175 

3.2497 

3. 00 11 

2.5340 

2.5°89 

2.484] 

2.4841 

3.2822 

3.2822 

3 .. 2497 

3 .. 24g7 

3.2497 

3.3482 

3 .. ,482 

2 .. 8840 

7..9128 

3.0311 

3.00 II 

2.8840 

2.8554 

2.689g 

2.6633 

2.7714 

2.7714 

3.519U 

2.6633 

2.61599 

3 .. 0U 11 

3.0311 

3 .. 4B41 

2.5u89 

2.5594 

3.1541 

3 .. 1229 

3.7355 

3 .. 3'+82 

3.3817 

3.4841 

3.UYZO 

3 .. U614 

3.282? 

3 .. 5547. 

3 .. 5542 

3 .. B 106 

3.2175 

3 .. 2497 

3.4841 

2.716!-J 

2.6633 

2 .. 5850 

3.31'JO 

3 .. 772B 

3.7355 

3.3150 

3.2822 

2 .. 7168 

2 .. 6633 

2 .. 6633 

3 .. 1541 

3 .. 1229 

2.6633 

2.6H99 

2.4B41 

2 .. 4H'tl 

3.1857 

3.1041 

3 .. 1229 

3.5542 

3.5190 

3 .. :,BY 7 

2.S/UH 

2 .. 'J594 

2.4841 

2.lll:l4U 

3. ')Sg I 

3 .. H411 1 

3 .. 3tH 7 

3. :>l9( 

3. ;:i4Hd 

j~31::'Ll 

:; .. 'J J YU 

3 .. 'J 19U 

3.0920 

3.u311 

ACTUAL 

3.214 

3.250 

3.000 

2.530 

2.505 

2.488 

2.488 

3.286 

3.288 

3.249 

3.250 

3.250 

3.346 

3.344 

2.884 

2 .. 91.? 

3.032 

3.00 I 

2 .. 884 

2.856 

2 .. 693 

2.659 

.? .. 77 2 

2.772 

3.518 

2.659 

2.6Y3 

3 .. 00 1 

3.034 

3 .. 488 

2.508 

2.555 

3.155 

3.126 

3.735 

3 .. 345 

3.383 

3.488 

3.092 

3.058 

3.2B4 

3 .. :'52 

3 .. 552 

34008 

3.221 

3.246 

3.486 

2. 7J 5 

2 .6~9 

2.585 

3.314 

34776 

3.736 

3.312 

3.285 

2.728 

2.6:'9 

2.660 

3.1'31 

3 .. 124 

2 .. 661 

2.689 

2.4B8 

2~ 4Hh 

3.lB9 

3 .. 151 

3.119 

34556 

3.519 

3 .. 593 

2.911 

2.556 

2~487 

2.888 

3 .. 509 

3.845 

3.385 

3.510 

3.345 

3a 31 7 

3.516 

3.518 

3 .. 091 

3. U29 

DEG. ANGU' 

1 .. 0 8.50B 

1 .. 0 5.672 

1.0 30 .. 487 

1.5 38 .. 995 

1.5 38.995 

1 .. 5 42.540 

1.5 42 .. 540 

1.0 -9.217 

1 .. 0 -9.217 

2.0 15 .. 591::1 

2.0 15.598 

1.5 16.107 

2 .. 5 15.~9l:1 

2 .. :, 1"i .. ~; q 1::1 

3.0 -29.D6'J 

3.0 -29.069 

3 .. 5 -7.090 

3.5 -7.090 

3.5 -4.~<)4 

3.5 -4.?~4 

3.0 -4.254 

3.0 -4.2')4 

1 .. 0 ?9,"I7H 

1.0 2'-1.'7'11;< 

I.e ? .. 12 7 

1 .. 0 -37.'.., (( 

1 .. 0 -37 .. 577 

1.0 -27 .. hI) 1 

1.0 -27.f.~1 

1.5 -lR.434 

1 .. 0 -4?~40 

1.0 -42.:',4U 

2 .. 0 24.106 

2.0 24.106 

2 .. 5 4 .. 2')lj2.~ -19~R'};; 

2.') -lY .. h")2 

2.0 20.'Jf>} 

2.') 2b .. 9!~.! 

2.5 26. Q '.2 

2.:) 1"'· .<, 1'-t 

3.0 -'-!. .. ')It") 

3.0 -1.',4:.> 

2 ~ -. (()9 

2.5 -26.2.D 

2.5 -2h.233 

3 .. 0 -13 .. f t71 

2..5 ":)6. Hr,(-l 

2.5 jb. 

2 .. 0 44.l:-oh7 

2. ') 264 ,! 3 3 

3 .. 0 4 .. ?"J'; 

3 .. 0 -13 .. ',71 

3.5 ? .. J? I 

3.5 2 .. 1 ;0'( 

3 .. 0 30.'+tl-! 

3 .. 0 '-3n .4(j { 

2.5 36.Hhd 

3.'3 b. Hll 

3.5 6.1Rl 

3 .. 0 -34.032 

3 .. 0 -34 .. 052 

0 .. 0 -41.9SK 

0.0 -t.ja9SA 

1 .. 5 29.7 7l:1 

2 .. 0 24.106 

2 .. 0 24.106 

2.5 ':1.1>72 

2 .. 5 ::, • ~-. 1/ 

2.5 -2.1/7 

2 .. 0 37.614 

2 .. 0 43.749 

2 .. 0 43. 2<tl} 

2.5 -<.?'-J4D 

3 .. 0 -24.106 

3 .. D -14~ lRO 

340 -24.81') 

3.0 -13 .. '-t71 

3.0 17~D16 

3aO 17.016 

3.5 -8.503 

3.5 -8.008 

3.0 24.H15 

3.0 24.8 b 

A-17 

Approved for Release: 2018/09/11 C051 03025 
I BCS 39739-65 

PERFORMANCE EVALUATION TEAM I REPORT NO. 4022/65 

COMMAND INFORMATION 

Handle via Byeman 

Controls Only 

I ACC. 

rw. SY ST E;,1 T UH:. 

bUR::' T 

T I f.!E 

COI-ir-lAi-JD pOSITroN 

LAT LONG 

8EST EPHEMERIS FILM VELOCITY IN./SEC. l"JRROR 

CRAB ROLL 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

REV 056 

1 

2 

10 

11 

12 

13 

14 

10 

16 

17 

18 

19 

20 

21 

22 

23 

24 

25 

R!-V D57 

1 

2 

" 7 

8 

9 

10 

11 

12 

13 

14 

15 

16 

17 

18 

19 

20 

21 

22 

SEC 

22088.81 

22105.31 

22197.41 

22223.61 

22234.91 

22252.11 

22263.41 

22405.51 

22432.21 

2 2 /t44 .. 31 

22474 .. 21 

22501.71 

22~13 .. 01 22:;37.51 

22549.21 

22590.21 

22601 .. 91 

22613.61 

22660 .. 41 

22672.91 

22697.31 

22719 .. 41 

22737 .. 81 

22770.61 

22785.21 

27369 .. 81 

27333.91 

27518.41 

27530.11 

27560.01 

27572 .. 11 

27585.41 

27717.61 

27729.11 

27745 .. 31 

27761 .. 51 

27783.41 

27795.51 

27811.31 

27323 .. 41 

27850.91 

27861.31 

27887.41 

27986.21 

27997.51 

28199 .. 31 

28211 .. 41 

SeC 

5.1 

5.1 

5.1 

:> .9 

5 ~ 9 

5.9 

5.9 

6.2 

5.5 

7.1 

5.1 

7.4 

7.8 

6 .. 3 

6.3 

5.4 

:'.4 

7.7 

5.9 

5.9 

6.3 

5 .. 3 

5.4 

9.1 

9.0 

7 .. '..1 

7 .. 5 

6.3 

6.3 

7.9 

7.9 

5 .. 6 

7.7 

6.0 

1 [. 3 5 .. ., 

6.6 

6.2 

5.5 

6.0 

6,.7 ".7 

6.3 

5.9 

0.9 

5.5 

5.5 

Handle via Byeman 

Controls Only 

DcG 

7~ 

71 

69 

67 

57 

55 

55 

52 

51 

50 

48 

45 

',4 

43 

40 

37 

36 

34 

32 

31 

80 

71 

68 

67 

58 

57 

56 

55 

53 

52 

51 

51 

49 

46 

39 

25 

.~;[N DEG 

31N 

4/:1N 

55N 

38N 

SON 

DON 

59N 

06N 

20N 

40N 

04N 

16N 

28N 

16N 

45N 

14N 

58N 

43N 

43N 

43N 

33N 

49N 

08N 

16N 

29N 

24N 

18N 

49N 

59N 

55N 

OSN 

13N 

44N 

59N 

2H~ 

103 

91 

~9 

88 

82 

82 

31 

81 

80 

60 

79 

78 

78 

78 

77 

71 

76 

76 

76 

75 

89 

69 

66 

65 

60 

60 

60 

59 

59 

58 

58 

58 

57 

5"1 

55 

52 

1·1IN 

19E 

38E 

57< 

23E 

44E 

02 E 

44E 

02E 

26E 

12E 

43E 

45E 

33E 

21E 

36E 

02E 

43E 

27E 

DOE 

48E 

31E 

29E 

55E 

37E 

49E 

30E 

04E 

39E 

08E 

52E 

3lE 

15E 

42E 

OOE 

2IE 

26E 

OEG 

78 

77 

71 

69 

69 

67 

67 

57 

55 

55 

52 

51 

50 

48 

47 

45 

44 

43 

40 

39 

37 

36 

34 

32 

31 

80 

79 

71 

70 

68 

68 

67 

58 

57 

56 

55 

53 

53 

51 

51 

49 

48 

46 

39 

39 

25 

24 

LAT LONG 

23 .. 58N 

23.46N 

31. 72N 

48.72N 

4 .. 05N 

55.82N 

10.85N 

38.8 IN 

50.40N 

1 .. 20N 

59.46N 

7 .. 30N 

21.17N 

41.05N 

53.2aN 

5.34N 

17.39N 

29.42N 

17.36N 

26 .. 0iN 

45 .. 73N 

14.851\1 

59.16N 

44 .. 14N 

'.4.02N 

43.84N 

56.50N 

33 .. 70N 

47.S1N 

49.81N 

1.79N 

3 .. 86N 

16 .. 90N 

30.26N 

24 .. 50N 

18.65N 

49.53N 

.23N 

55.BIN 

6.44N 

14.11 N 

29.55N 

4'-t- .. 81N 

59 .. 62N 

13 .. 20N 

22 .28N 

32.38N 

DEG 

103 

100 

91 

89 

89 

88 

87 

82 

82 

81 

81 

80 

80 

79 

79 

78 

78 

78 

77 

77 

77 

76 

76 

75 

75 

89 

86 

69 

6S 

66 

66 

65 

60 

60 

60 

59 

59 

58 

58 

58 

57 

57 

57 

55 

55 

52 

52 

MrN 

19.5bE 

47 .. 32E 

37.92E 

56.74E 

17.70E 

22.77E 

49.29E 

43 .. 75E 

1.85E 

43 .. 91 E 

2.07E 

26 .. 30E 

12.28E 

43.05E 

29.63 E 44 _ 9 7 E 

32.84E: 

20.95E 

35.62E 

24.05E 

2 .. 04E 

42.72E: 

?7 .02E 

59.87E 

48.08E 

33 .. 27E 

12.18E 

29.39E 

42.04E 

55. lIE 

16 .. 68E 

37.17E 

48.60E 

29.59E 

3.92E 

39 e 47 E 

8 .. 1 3E 

51.58E 

30.73E 

15.29E 

41d8E 

29.04E 

.. 24E 

ZO.83E 

lO./-t-3E 

26.19E 

17.29E 

-,. O~ SECRET - GAMBIT - Approved for Release: 2018/09/11 C051 03025 

comlAND 

2 .. 481~ 1 

2.4841 

2.8554 

3.1229 

3.1541 

3.1229 

3.1541 

2.4841 

3.1229 

3 .. 09 20 

3.0614 

3.1229 

3.1541 

3.2822 

3.2497 

3.2175 

3.2497 

3.1229 

2 .. B5~4 

2.9128 

3 .. 4841 

2 .. 6633 

2.9128 

2.8840 

2 .. 9128 

2 .. 6108 

2.7168 

2.9419 

2.9713 

3.0920 

3 .. 0614-

3.1229 

3. 62~6 

3.6619 

3.5542 

3.5190 

3.0920 

3.0920 

3.0920 

3 .. 0920 

3 .. 4496 

3.4496 

3.U920 

3 .. 21 75 

3 .. 2497 

3.0920 

3.1229 

ACTUAL 

2 .. 487 

2 .. 487 

2.B54 

3.125 

3.152 

3.124 

3 .. 158 

2.482 

3 .. 121 

3.091 

3.059 

3.[ 21 

3.151 

3.285 

3 .. 245 

3.215 

3 .. 246 

3.1 19 

2.851 

2.912 

3 .. 487 

2.661 

2 .. 908 

2.885 

2.908 

2 .. 609 

2.726 

2 .. 937 

2 .. 968 

3.092 

3.058 

3.117 

3 .. 624-

3 .. 6'J9 

3.550 

3 .. 518 

3.091 

3.091 

3.091 

3.091 

3.445 

3.449 

3.092 

3 .. 213 

3.249 

3.091 

3.! 19 

POS. DEG. ANGLE 

1..0 41.831 

1.0 41.R31 

1.0 3 f+ .. 741 

1.0 -18 .. 434 

1 .. 0 -lR .. 434 

1.0 -20 .. 561 

1.0 -20.:'61 

2 .. 0 It 1.122 

2.0 23 .. J97 

2 .. 0 13.397 

1.5 33.323 

2 .. 0 -,?7 .. 651 

2 .. 0 -27.651 

2.5 1Q.143 

2.5 19.143 

2.0 -25.524 

2.0 -2').',/.4 

2.0 -36.159 

2.0 -37.~)77 

2.0 -370577 

2~5 9.926 

2.5 ''-1.122 

2.5 34.741 

2.~ -lt2.5'tO 

2.5 -41. R 31 

1.0 32.614 

1.0 29.7713 

.5 -25 .. 524 

oS -2,)~5l4 

1.0 -21.979 

1.0 -24.815 

1.5 -22.688 

2.0 -12.762 

2.0 -8.508 

2 .. 0 14 .. 889 

2.0 16.307 

2.0 ?4.Hl' 

2.0 24.fl15 

2 .. 0 25.5?tt 

2 .. 0 25,.524 

2.5 90217 

2.5 9.217 

2.5 -31.196 

2.~ -26.233 

2 .. 5 -26.23.3 

3.0 -31.1G6 

3.0 -31.196 

A-18 
I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Ace. SYSTEM NO.. T HIe 

SEC 

REV 0;8 

32791.51 

32806. 4 1 

32943 .. 91 

32961.51 

32972.41 

6 32985.21 

7 33018.71 

33029.21 

33069 .. 11 

10 33080.41 

11 33100.31 

12 33110.81 

13 33143 .. 51 

14 33153 .. 61 

1') 33175 .. 21 

16 33185.71 

17 33225.31 

18 33236.21 

19 33442.81 

20 33453.71 

REV 059 

BURS r TIME 

SEC 

7.1 

7.1 

6.3 

5.5 

5.5 

5.8 

6.3 

6,3 

5 .. 9 

5 .. 9 

6.3 

6.3 

7.1 

7.1 

6.3 

6.3 

5 .. 5 

5.5 

5 .. 5 

5.5 

I 37998.71 5.5 

2 38010.81 5.5 

38419 .. 11 5 .. 3 

3843~.51 5 .. 0 

384'5':> .. 41 5 .. 4 

38465.41 19.3 

38487.91 5.1 

REV D63 

1 59376 .. 40 9.1 

59638 .. 00 60.1 

59827 .. 30 5.1 

59900.70 9.1 

60147.\0 7.9 60159.60 7.9 

R l: V 064 

1 64762 .. 50 

64818.30 

64934 .. 70 

6':)031 .. 40 

65042 .. 30 

6':.095.90 

b5106.80 

b'" 23,1. 51) 

6')240 .. 60 

10 6~339.40 

24 .. 8 

60 .. 1 

60 .. 0 

5.5 

5.5 

5.5 

5.5 

COfiMAND POS IT ION 

lAT l.ONG 

DEG MI N DfG 

74 40N 51 

64 39N 41 

63 29N 41 

61 53N 40 

59 38N 39 

56 14N 37 

54 07N 37 

51 liN 36 

49 01N 35 

45 36N 34 

30 42N 31 

81 27N 

54 17N 

53 ION 

51 49N 

51 08N 

49 36N 

75 50N 

58 34N 

45 42N 

40 41N 

23 46N 

22 55N 

71 

67 

60 

53 

49 

40 

39 

32 

35N 

55N 

08N 

35N 

12N 

OON 

19N 

32N 

48 

14 

14 

14 

13 

13 

57 

72 

76 

77 

80 

81 

B:;, 

89 

93 

96 

9g 

100 

101 

MIN 

18E 

48E 

08E 

17E 

13E 

49E 

03E 

06E 

27E 

32E 

15E 

59E 

56E 

33E 

07E 

54E 

27E 

37W 

08W 

20W 

34W 

55W 

04W 

43W 

03W 

37W 

llW 

33W 

5 3 ~/ 

03W 

2BW 

COMMAND INFORMATION 

BEST EPHEMERIS 

LAT LONG 

DEG MIN 

74 40.59N 

73 43.37N 

64 40 .. 36N 

63 29.68N 

62 45.83N 

61 54.25N 

59 38.93N 

58 56.43N 

56 14.56N 

55 28.63N 

54 7.66N 

53 24.90N 

51 11.55N 

50 30.32N 

49 2.07N 

48 19.13N 

45 37.04N 

44 52.38N 

30 43.19N 

29 58.28N 

81 27.58N 

80 48.87N 

54 17. 34N 

53 10.54N 

51 49 .. 40N 

51 8.60N 

49 36.71N 

75 50.BIN 

58 34.27N 

45 42.'t3N 

40 41.38N 

23 46.95N 

22 55.40N 

71 35.86N 

67 55.58N 

60 8.Z8N 

53 35.67N 

52 51.26N 

49 12 .. 45N 

48 27 .89N 

'to .. 83N 

39 19.34N 

32 32.95N 

DEG MIN 

51 18.91E 

49 55 .. 82E 

41 48.82E 

41 7.92E 

4D 44.0bE 

40 17 .34E 

39 13.19E 

38 54.60E 

37 49.45E 

37 32.39E 

37 3.63E 

36 49.07E 

36 6.13E 

35 53.54E 

35 27.56E 

35 15.36E 

34 31.62E 

34 20.14E 

31 14.76E 

31 6.20E 

49 1.17E 

45 36.86E 

14 56.25E 

14 33.54E 

14 7.23E 

13 54.48E 

13 26.86E 

57 31.61W 

72 8.41W 

76 20.43W 

77 33.84W 

80 54.88W 

81 3.91W 

85 43.26W 

89 3.00W 

93 37.68W 

96 11.33W 

96 26.12W 

97 33.43W 

97 46.15W 

99 53.59W 

100 2 .. 89W 

101 27.79W 

Handle via Byeman 

Controls Only T~T-GAMBIT 

Handle via Byeman 

Controls Only 

FILM VELOCITY IN./SEC. MIRROR 

CRAB ROLL 

COMMAND 

2.4841 

2.4841 

3.1541 

3.3817 

3.3817 

3.6619 

3.2822 

3.3150 

3 .. 3817 

3.3817 

3.4155 

3 .. 4496 

3.4841 

3.4841 

3.4496 

3.4841 

3.4155 

3 .. 4496 

3.3462 

3.3817 

3 .. 0920 

3.1229 

3.3617 

3.3482 

3.7355 

3.5190 

3.7728 

3.3482 

3 .. 6985 

3.5897 

3.')897 

2.8554 

2.9128 

3.3817 

3.3482 

3 .. 4155 

3.4155 

3 .. 4496 

3.3817 

3.4155 

3.5542 

3.5190 

3.8106 

ACTU~L 

2.486 

2.485 

3.[ 53 

3.378 

3.378 

3.658 

3.281 

3.310 

3 .. 381 

3.383 

3.413 

3.445 

3 .. 487 

3.487 

3.448 

3.485 

3.414 

3.448 

3.346 

3.378 

3.094 

3.122 

3 .. 382 

3.346 

3.733 

3.522 

3.773 

3.341 

3.696 

3 .. ~91 

3.591 

2.855 

2.910 

3.381 

3 .. 345 

3.41B 

3.418 

3 .. 448 

3.384 

3.412 

3.552 

3.521 

3.816 

POS. DEG. 

1.0 

1.0 

1.0 

1.5 

1.5 

1.5 

1.5 

1.5 

2 .. 0 

2.0 

2.0 

2.0 

2.0 

2.0 

2.5 

2.5 

2.5 

2.5 

3.0 

3.0 

ANGLE 

39.704 

39.704 

-29.778 

-1.418 

-1.418 

0.000 

-17.725 

-17.725 

9 .. 926 

9.926 

-10.635 

-10.635 

-7.090 

-7, 090 

-11 .. 344 

-11.344 

-17.016 

-17.0\6 

-21.270 

-21.270 

.5 9.217 

.5 9.217 

2.0 -26.233 

2.0 -27.651 

2.0 0.000 

2.0 -2.836 

2.0 -4.254 

.5 -15.598 

2.0 -4.254 

2.0 17.016 

2.5 16.30-' 

2.5 -36.868 

2.5 -36.868 

0.0 -6.381 

1.5 -8.508 

2.0 -9 .. 217 

2 .. 0 -12.762 

2.0 -12.762 

2.0 -17.725 

2.0 -17.725 

3.0 2.836 

3.0 2.1336 

3.0 2.B36 

Approved for Release: 2018/09/11 C051 03025 

A-19 
~ 

I A2proved 

~ ~~~~~~ 

for Release: ~ 2018/09/11 ~~~~.~~~-C051 03025 Handle via Byeman 

BCa 39739-65 Controls Only 

PERFORMANCE EVALUATION TEAM 

I REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I Ace. NO. DENSITY DENS lTV SUN ANGLE BRIGHTNESS CLOUD ALTITUDE 

OHIN DHAX BASE + FOG !DEGREES' RANGE DMAX eN"" 

REV D 4 

1 .45 1.73 .13 17 3.75 96.2 

I 2 .41 1.72 .14 17 4.02 95.8 

3 .68 1.98 .22 17 4.04 95.5 

4 .79 1.20 .12 24 1.44 1.53 93.0 

5 .98 1.42 .22 24 1.5" 1.90 92.7 

6 .S8 1.08 .22 35 1.21 2.52 88.9 

7 .94 1.28 .22 35 1.38 2.52 88.7 

I REV D 

1 .56 1.90 .22 13 4.15 1.60 96.2 

2 .56 1.87 .22 13 3.99 1.45 97.2 

3 .12 27 1.68 91.8 

4 .10 27 1.61 91.5 

I 5 .42 1.21 .22 33 2.60 2.03 89.6 

6 .43 1.20 .22 33 2.53 2.25 89.3 

7 .43 1.42 .22 37 3.17 1.57 88.2 

8 .57 1.50 .22 39 2.62 2.32 87.7 

9 .34 .90 .22 42 2.46 87.! 

10 .46 .94 .22 43 1.86 2.32 86.8 

11 .52 1.14 .22 43 1.99 2.32 86.6 

I 12 .29 1.16 .22 45 3.75 86.2 

13 .35 1.32 .22 45 3.56 86.0 

14 .36 1.30 .22 47 3.36 85.8 

15 .35 1.55 .22 47 4.52 1.30 85.6 

16 .12 79 1.76 89.9 

17 .12 79 1.82 9003 

I REV o 6 

1 .76 1.58 .ll 13 2.13 1.41 96.2 

2 .36 1.40 .11 13 3.56 1.32 97.2 

3 .10 33 1.72 89.5 

4 .20 35 1.98 89.2 

5 .22 34 1.93 88.9 

I 6 1.01 1.48 .21 47 1.60 2.06 85.6 

7 .62 .99 .12 47 1.46 1.74 85.4 

8 .11 51 1.34 85.0 

9 .10 54 1. 56 84.6 

10 .10 54 1.60 84 .. 6 

11 .42 .97 .21 57 2.08 2.16 84.4 

I 12 .32 .87 .22 59 2.56 2.32 84.3 

13 .28 1.28 .21 61 4.57 2.2S 84.3 

14 .40 .98 .21 61 2.19 2.28 84.3 

15 .81 .97 .21 63 1.17 2.01 84.4 

16 .32 .82 .22 64 2.43 2.28 84.4 

17 .60 .72 .22 79 1.15 2.30 88.2 

16 .55 .70 .22 79 1.20 2.22 86.5 

I 19 .49 1.72 .21 78 3.88 2.20 89.2 

20 .39 1.70 .23 78 4.66 1.91 89.5 

REV D 

1 .28 1.04 .21 9 3.63 1.39 96.2 

2 .57 .97 .21 9 1.55 1.09 99.2 

.21 14 1.80 97.3 

I 4 .56 .97 .21 14 1.57 1.89 96.8 

5 .21 26 1.18 92. I 

b .21 28 2.20 91.5 

7 .60 .93 .21 28 1.44 1.78 91.2 

8 .40 .52 .21 30 1.28 1.84 90.8 

9 .1l 31 2.00 90.2 

10 .11 31 2.00 89.9 

I 11 .11 32 1.89 89.4 

12 .60 1.24 .21 36 1.93 2.39 88.,6 

13 .45 1.02 .ll 35 1.90 2.28 88.4 

14 .11 44 1.45 86.5 

15 .10 44 l.bO 86.3 

16 .44 1.42 .21 56 3.11 2.06 84.5 

17 .40 1.40 .21 56 3.30 2.00 84.5 

I 18 .34 1.96 .21 70 7.57 1.82 85.2 

19 .48 1.76 .21 70 4.14 1.78 85.3 

20 .4(} 1.82 .21 75 5.21 1.87 86.5 

21 .36 .84 .21 75 2.16 1.87 86 .. 7 

REV o 8 

I 1 .35 .78 .22 6 2.09 1.31 96.2 

2 .36 1.06 .22 6 2.67 1 .. 04 100.3 

3 .22 8 1.80 99 .. 6 

4 .22 8 1.66 99.2 

5 .65 1.50 .22 29 2.39 2.06 90 .. 7 

.48 1.15 .22 30 2.18 2.36 90.4 

I .60 1.24 .22 30 1.93 2.36 90.1 

8 .10 35 1.66 88.8 

9 .10 35 1.76 88 .. 4 

10 .69 1.46 .22 40 2.19 2.16 87.2 

11 .66 1.64 .22 40 2.75 2.14 87.0 

12 .52 1.82 .22 46 4.08 85.8 

13 .44 1.74 .22 47 4.40 85.6 

I 14 .66 1.32 .22 48 1.95 1.70 85.3 

I'> .42 1.22 .22 50 2.63 85.1 

16 .34 1 .. 44 .22 51 4.17 85.0 

17 .44 1.52 .22 51 3.45 84.9 

I Handle via Byeman 

~T 

A-20 

Controls Only - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 
I .A2Pio~ed lo.!:... R~I~~~: .?018/0~! !"~Q~ Q3il25 Handle via Byeman 

BCS 39739-65 Controls Only 

I PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I ACC. NO. DENSITY DENS lTV SUN ANGLE BRIGHTNESS CLOUD ALTITUDE 

OMIN DHAX BASE + FOG IDEGREESl RANGE DMAX INMl 

REV o 9 

I 1 .46 .78 .22 5 1.58 1.68 96.2 

2 .38 .14 .22 5 1.80 1.30 100.5 

3 .94 2.14 .22 8 3.82 2.01 99.4 

4 .86 1.82 .22 8 2.67 2.08 99.0 

5 .42 2.22 .22 II 8.88 91.9 

6 .86 1.86 .20 13 2.19 1.96 91 .. 4 

7 .16 1.76 .20 12 2.80 1.90 97.0 

I B .11 14 1.26 96.5 

9 .12 15 1.38 96.! 

10 .11 18 1.56 94 .. 9 

11 .10 18 1.42 94.6 

12 .66 .76 .13 21 1.13 2.10 91.6 

13 .40 1.03 .12 27 2.12 2.34 91.2 

I 14 .20 30 2.36 90 .. 4 

15 .12 30 2.16 90,[ 

16 .10 33 1.81 89.2 

17 .60 1.32 .22 34 2.09 2.24 88.9 

16 .12 1.26 .20 34 1.75 2.14 88.6 

19 .65 1.13 .20 36 3.07 2.42 88.3 

20 .34 1.52 .20 37 4.54 88.0 

I 21 .38 1.58 .20 37 4.21 81.8 

22 .32 .78 .20 40 2.32 87.1 

23 .30 1.10 .20 41 3.41 1.68 86.7 

24 .26 1.42 .20 43 6.29 86.5 

25 .28 1.56 .22 43 6.13 1.82 86.3 

26 .27 .92 .21 44 3.54 2.00 86.0 

27 .42 1.50 .20 49 3.52 B5.4 

I 2B .46 1.66 .20 49 3.86 85.2 

29 .74 1.54 .20 53 2.24 1.62 84.7 

30 .75 1.60 .20 65 2.96 84.5 

31 .60 1.42 .20 65 1.85 84Gb 

32 .68 1.35 .12 66 1.61 1.25 84.8 

I REV 010 

1 .21 3 1.05 96.2 

2 .21 3 .72 101.2 

3 .37 1.58 .22 17 4.36 2.10 95.6 

4 .37 1.50 .22 16 4.01 2.06 95.3 

5 .58 1.20 .22 18 1.90 2.20 94.7 

6 .38 .65 .22 19 1.62 2.15 94.2 

I 7 .32 .80 .22 23 2.31 2.10 92 .. 9 

.32 1.48 .22 23 4.66 1.98 92.6 

9 .34 1.20 .22 25 3.26 92.1 

10 .42 1.35 .22 25 3.01 91.8 

II .34 1.18 .22 27 3.20 2.12 91.4 

12 .39 1.21 .22 27 2.71 2.10 91.1 

I 13 .60 1.60 .22 21 2.81 2.40 90.7 

14 .47 1.10 .22 29 2.12 2.18 90.4 

15 .49 1.38 .22 29 2.69 2.34 90.1 

16 .40 1.45 .22 31 3.48 2.20 89.7 

17 .46 1.58 .22 31 3.53 2.15 89.4 

18 .45 1.52 .21 33 3.38 88.9 

19 .44 1.58 .22 35 3.68 88.5 

I 20 .50 2.20 .22 36 1.29 88.1 

21 .32 1.20 .22 36 3.49 87.9 

22 .44 1.50 .22 37 3.38 87.7 

23 .44 1.71 .22 38 4.54 87.4 

24 .37 1.26 .22 38 3.12 87.2 

25 .26 1.15 .22 42 4.78 86 .. 6 

26 .29 1.32 .22 42 4.40 86.5 

I 27 .31 1.15 .22 44 3.45 86.1 

28 .33 1.12 .22 44 3013 86.0 

29 .36 1.42 .22 71 3.81 85.6 

30 .48 1.50 .22 11 3.11 85.7 

31 .42 .58 .22 75 1.36 2.06 86.5 

32 .36 .75 .22 15 1.95 2.26 86.8 

33 .36 .70 .22 76 1.84 2.24 81.5 

I 34 .38 .80 .22 76 1.93 2.05 87.7 

35 .50 .66 .22 77 1.27 2.28 88.1 

36 .62 .88 .22 17 1.34 2.28 88.4 

37 .. 22 78 2.22 88.7 

38 .12 79 1.69 90.6 

39 .12 79 1.65 91.1 

40 .12 80 1.62 91.4 

I REV 011 

1 .34 2.16 .21 7 10.11 1.99 96.2 

2 .41 1.99 .20 1 6.37 1.87 99.2 

3 .39 .99 .21 24 210 26 92.7 

I 4 .40 1.10 .20 24 2.45 92.3 

5 .46 1.00 .20 26 1.91 2.18 91.9 

.49 1.16 .21 26 2.15 2.22 91.5 

.54 1.12 .21 27 1.88 91.1 

.49 .80 .21 41 1.52 2.32 86 .. 9 

.54 1.13 .20 41 1.89 2 .. 35 86.7 

I 

I Handle via Byeman 

~ A-21 

Controls Only - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 
~ 

I ~:1.ed f;!r...R.:J~~~ ~018/0~11..S2~2.3.225 Handle via Byeman 

BCS 39739-65 Controls Only 

I 

PERFORMANCE EV ALUA TION TEAM 

REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I ACC. NO. DENSITY DENS lTv SUN ANGLE BRIGHTNESS CLOUD ALTITUDE 

OMIN DMAX BASE + FOG IDEGREES) RANGE DMAX INMI 

REV 013 

I I .36 1.36 .20 59 3.58 96.2 

2 .37 10 51 .20 59 4.05 107.4 

3 .34 1.49 .21 58 4.40 108.0 

4 .52 2.03 .21 53 5.39 !l2.0 

5 .49 1.72 .21 53 3.88 112.7 

I REV 014 

I .34 .92 .21 6" 2.51 2.26 96.2 

2 .40 .94 .21 6" 2011 2.30 84.,6 

REV 015 

1 .30 1.12 .22 39 3."7 96.2 

I 2 .32 1.15 .22 39 3.33 86.8 

3 .35 1.46 .22 41 4.12 86.6 

4 .36 1.52 .22 40 ".23 86.,4 

5 .36 1.34 .22 44 3.51 85.9 

6 .34 1.50 .22 4'. 4.44 85.7 

7 .27 1.10 .22 46 4019 85.4 

8 .28 1.10 .22 48 3.8" 85.2 

I 9 .25 .82 .22 50 3.83 .B5 84.9 

9 .14 50 1.64 84.9 

9 .12 50 1.38 84.9 

REV 016 

1 .38 .98 .21 33 2.31 2.10 96.2 

I 2 .48 1.09 .20 37 2.06 1.57 87.5 

3 .30 1.40 .20 44 4.59 85.7 

4 .30 1.20 .21 48 3.74 85.1 

5 .36 1.28 .21 48 3.29 85.0 

.41 1.44 .21 50 3.37 84.8 

.48 1.42 .21 51 2.86 84.7 

I REV 017 

1 .44 1.80 .21 73 4.70 2.26 96.2 

2 .33 1.89 .20 73 7.11 2.28 98.1 

I REV D19 

.51 2.16 .22 21 6.61 2.25 96.2 

.56 2.10 .22 21 5 .. 48 2.26 92.0 

REV 020 

1 .51 2.26 .12 16 6.75 96.2 

2 .58 2.22 .12 16 5.77 94.2 

I 3 .57 .80 .13 24 1.32 1.92 91.0 

.12 27 2.10 90.4 

.12 27 2.02 90.! 

.12 27 1.52 89.9 

.10 30 1.84 89.4 

8 .12 30 1.76 89.1 

I 9 .48 1.95 .12 33 4.56 2.20 88.3 

10 .75 1.20 .20 33 1.56 2.40 88.! 

REV 021 

1 .43 1.74 .23 15 4."9 96.2 

2 .38 1.69 .23 15 4.76 94.3 

I 3 .49 1.31 015 26 2.32 1.67 90.5 

4 .70 .93 .15 26 1.24 2.10 90.2 

5 .35 1.72 .23 35 5.46 2.07 87.6 

.37 1.52 .22 35 4.09 2.17 87.4 

.44 1.38 .23 37 2.98 1.10 87.0 

8 .72 1.63 .23 38 2.53 86.7 

9 .47 1.15 .23 39 2.22 86.5 

I ID .43 1 .. 44 .23 42 3.24 86.0 

11 .46 1.52 .23 42 3.31 85.9 

12 .15 78 2.16 88.6 

13 .14 78 1.62 88.9 

14 .71 .99 .22 78 1.34 2.04 89.4 

15 .46 .73 .23 80 1.49 2.36 90.7 

16 .50 .80 .22 80 1.49 2.40 91.2 

I 17 .48 1.92 .23 79 5.02 2013 91.5 

18 .47 1.97 .23 79 5.49 2.13 92.0 

I 

I 

I Handle via Byeman 

~T 

A-22 

Controls Only - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 
I ~o1ed!~ ~~e~: ..?018/0~11S2~2~025 Handle via Byeman 

BCB 39739-65 Controls Only 

I 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I ACC. NO. OENSI TY DENS I TV SUN ANGLE BRIGHTNESS CLOUD ALTITUDE 

OMIN DMAX BASE + FOG (oEGRE E S) RANGE DMAX INM) 

REV 022 

I 1 .23 14 2.11 96.2 

2 .13 14 1.85 94.8 

3 .20 17 1.65 93.8 

4 .21 17 1.55 93.5 

5 .50 1010 .21 19 2.00 1.90 93.1 

6 .47 .88 .21 19 1.73 1.12 92.7 

I 7 .50 2.11 .21 28 6.27 2.31 90.0 

8 .64 2.22 .21 28 6.10 2.10 89.6 

9 .92 1.28 .21 35 1.41 1.93 87.7 

10 .56 1.19 .12 35 1.89 1.78 87.5 

II .40 1.23 .21 46 2.76 1.93 85.3 

12 .41 1.35 .20 46 3.07 1.96 85.2 

13 .36 .95 .21 47 2.41 2.01 85.0 

I 14 .40 1.11 .21 47 2.47 2.08 84.9 

15 .Il 49 1.29 84.7 

16 .Il 52 1.62 84.4 

17 .ll 55 1.45 84.3 

18 .46 1.16 .21 60 2.29 2.10 84.3 

19 .36 1.33 .20 60 3.47 2.20 84.4 

20 .31 1.55 .21 62 5019 2.22 84.4 

I 21 .36 1.65 .21 63 4 .. 88 2.00 84.5 

22 .40 1.58 .20 65 3.99 2.10 84.7 

23 .40 1.45 .21 66 3.48 2.21 84.8 

24 .80 .95 .21 78 1.17 2.14 90.6 

25 .77 I.ll .21 78 1.40 2.22 90.9 

26 .61 1.10 .13 79 1.63 2.14 91.6 

I REV 023 

1 .21 9 1.64 96.2 

2 .13 12 1. 57 96.1 

3 .21 12 1.57 95.7 

4 .32 1.56 .21 14 5.07 94.8 

I 5 .47 .73 .12 29 1.41 2.09 89 .. 2 

.66 .90 .12 29 1.28 1.82 88.9 

.69 1.37 .20 44 1.99 1.87 85.4 

.66 1.70 .21 44 2.94 1.66 8503 

9 .28 1.42 .21 56 5.29 2.10 84 .. 3 

10 .33 2.36 .21 57 15.23 2.07 84.3 

II .31 1.23 .21 59 3.72 1.91 84.3 

I REV 024 

I .21 ].10 96.2 

.27 .67 .21 6 2.69 1.05 97.8 

.21 8 1.54 97.2 

.21 8 1.18 96.8 

I 5 .48 .68 .21 16 1.35 1.95 94 .. 2 

6 .47 .76 .Zl 16 1.51 2.12 93.9 

7 .82 1.28 .21 31 1.56 2.16 88.8 

8 .76 1.43 .21 31 1.95 2.21 88.5 

9 .72 1.00 .13 35 1.29 2.12 87.5 

10 .30 .90 .ll 34 2.48 1.75 87.3 

II .Il 37 1.78 86.8 

I 12 .86 1.68 .22 38 2.28 86.,6 

13 .94 1.80 .21 38 2.42 86.4 

14 .30 1.00 .21 43 3.10 85.8 

15 .47 1.39 .21 43 2.83 85.6 

16 .39 1.09 .21 44 2.48 1.58 85.4 

17 .45 1.39 .21 46 2.95 85.0 

18 .35 1.45 .21 53 4.07 84 .. 4 

I 19 .46 1.50 .21 53 3.24 84.3 

20 .36 1.35 .21 10 3.54 2.08 100.0 

21 .30 1.45 .20 70 4.84 2.0L. 100.5 

I 

I 

I 

I 

I Handle via Byeman 

~ET A-23 

Controls Only - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 
~ 

I ~d !'0l... ~I~~~: lO18/O~11S2~23225 Handle via Byeman BCS 39739-65 Controls Only 

I 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I Ace. NO. DENS ITY DENSITY SUN ANGLE BRIGHTNESS CLOUD AlT !TUDE 

DMIN OMAX BASE + FOG I DEGREE S I RANGE OMAX I NM I 

REV 025 

I 1 .20 5 1.26 96.2 

2 .20 5 1.08 97.9 

3 .20 B 1.70 96.9 

4 .20 8 1.58 96.6 

5 .74 1.05 .20 9 1.37 1.55 96.2 

6 .72 2.08 .20 16 4 .. 43 2.25 93.8 

1 .46 1.5B .20 18 3.53 92.7 

I 8 .10 26 1.6B B9.9 

9 .10 26 1.48 89.6 

10 .56 1.63 .20 30 3.05 2.32 88.8 

II .58 1.32 .22 30 2.14 2.3B 88.6 

12 .52 1.53 .20 32 2.96 2.22 B8.2 

13 .41 .74 .11 33 1.43 1.75 87.8 

14 .45 .12 .11 33 1.45 1.64 87.5 

I 15 .75 1.57 .20 37 2.29 2.22 86 .. 9 

16 .94 1.70 .20 37 2.16 2.30 B6.7 

17 .46 1.00 .20 41 1.97 85.8 

18 .50 1.14 .20 41 2.07 85.7 

19 .35 1.62 .20 42 4.89 85.5 

20 .33 1.66 .20 44 5.47 85.3 

21 .. 26 1.16 .20 46 4.83 85.1 

I 22 .30 1.23 .20 46 3.85 85.0 

23 .44 1.40 .20 50 3.04 1.90 84.6 

24 .50 1.38 .20 50 2.64 2.02 8486 

25 .52 1.46 .20 52 2.75 1.90 84 .. 4 

26 .70 1.35 .20 52 1.93 2.04 84 .. 4 

27 .10 53 1.44 84.3 

I 28 .33 1.68 .20 66 5.60 1.90 84.9 

29 .56 1.42 .20 67 2.44 2.31 85.1 

3D .47 1.64 .20 72 3.70 2.34 86.7 

31 .44 1.30 .20 12 2.74 2.22 87.0 

32 .50 1.10 .20 77 2.00 2.34 88.2 

33 .68 1.03 .20 71 1 .. 44 2.24 88.5 

34 .40 1.30 .20 80 2.97 2.28 91.7 

I 35 .44 1.56 .20 80 3.60 2.37 92.2 

36 .57 1.40 .20 73 2.36 2.33 91.1 

37 .42 1.00 .20 73 2.14 2.28 97.6 

38 .53 1.58 .20 71 3.06 98 .. 4 

39 .50 1.52 .20 71 3.05 98.9 

40 .76 2.04 .20 70 4.00 2.24 99.8 

41 .30 1.70 .20 70 6.35 2.24 100.4 

I 42 .40 1.84 .20 67 5.33 2.32 102.3 

43 .33 1.78 .20 67 6.26 2.15 102.9 

44 .63 1.80 .20 64 3.40 2.30 104.5 

REV D26 

I .22 .38 .20 3 4.02 .82 96.2 

I 2 .24 .38 .20 3 2.28 .68 98.8 

3 .28 .48 .20 4 1.85 .90 98 .. 3 

4 .20 16 1.84 93.5 

5 .21 16 2.06 93.2 

.30 1.14 .21 18 3.54 1.78 92.5 

.52 .91 .21 21 1.61 2.28 91.8 

8 .52 1.80 .14 21 3.61 2.10 91.5 

I 9 .28 .74 .21 24 2.67 90.6 

10 .30 .. 54 .21 25 1.85 1.54 90.3 

11 .31 .62 .21 25 1.99 1.82 90.1 

12 .36 1.32 .21 27 3.43 1.16 89.6 

13 .43 1.40 .21 27 3.10 1.92 89.3 

14 .54 1.38 .20 28 2.43 1.50 89.1 

I 15 .45 1.50 .21 29 3.31 88.8 

16 .32 1.23 .21 32 3.59 2.32 88.1 

17 .37 1.20 .21 32 2.94 2.16 87.9 

18 .32 1.64 .21 34 5.54 1.80 81. 5 

19 .39 1.20 .21 35 2.15 2.10 87.3 

20 .45 1.22 .21 35 2.47 2.12 87.1 

21 .60 1.28 .21 36 2.01 1.87 86.9 

I 22 .39 1.01 .21 39 2.30 86.4 

23 .28 .94 .21 40 3.31 2.01 86.1 

24 .32 .98 .21 41 2.84 85.9 

25 .53 1.72 .21 42 3.58 85.7 

26 .34 .90 .21 42 2.""6 85.6 

27 .34 1.20 .21 43 3.26 85.4 

28 .27 .89 .21 44 3.44 85.3 

I 29 .11 17 1.34 88.0 

30 .Il 71 1.67 88.4 

31 .34 .65 .21 78 1 .. 86 2.10 90.3 

32 .34 .58 .21 78 1.72 2.00 90.6 

33 .11 78 1.72 91.5 

34 .11 78 1.51 91.8 

35 .43 .89 .21 17 1.89 2.14 92.9 

I 36 .38 .72 .21 77 1 .. 76 2.00 93.3 

37 1.24 1.74 .21 75 1.71 1.26 94.7 

38 .97 1.58 .21 75 1.84 1.14 95.2 

39 .48 1. 33 .13 75 2.40 1.70 95.6 

40 .78 1.40 .21 75 1.85 1.90 96.0 

41 .38 1.52 .21 73 3.95 2.02 97.0 

42 .34 1.51 .21 73 4.49 2.12 97.5 

I 

I Handle via Byeman A-24 

Controls Only TOp SECRET - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 
I ~d U.L..i'\,...t.i.\,..r...J.I.. 

for Release: 2018/09/11 - "-"II,S,.l..J.1'..I..LJ.L.a.. C051 03025 Handle via Byeman 

BCS 39739-65 Controls Only 

I 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I Ace. NO. DENSITY DENS !TY SUN ANGLE BRIGHTNESS CLOUD AL Tl TUDE 

OMIN OM AX BASE + FOG I DEGREE S I RANGE DMAX IN'" 

REV un .13 17 1.80 96.2 

I .13 17 1.63 93.1 

.62 1.04 .21 18 1.56 2.06 92.9 

.51 1 0 21 .21 18 2.17 2.00 92.5 

.12 23 1.35 90 .. 9 

.12 23 1.22 90.6 

.12 25 1.59 90.2 

.12 26 1.66 89.9 

I 9 .12 26 1.62 89.6 

ID .. 72 1.88 .22 37 3.36 2~42 86 ~ 8 

11 .76 2.0D .20 37 3.78 2.42 86 .. 6 

12 .32 1.86 .21 51 7.08 2 .. 30 84 .. 5 

13 .40 2.66 .21 51 59.57 2.28 84.5 

14 .62 1.78 .21 54 3.36 84.3 

I 15 .40 1.44 .23 54 3.44 84 .. 3 

REV lJ29 

1 .36 1.18 .20 57 2.98 96.2 

.33 1.32 .22 57 3.81 111.2 

.40 1.90 .21 54 5.74 112.8 

I .38 1.20 .22 54 2.84 113.7 

REV 031 

1 .44 1.82 .20 42 4.80 96.2 

2 .26 .96 .20 43 4 .. 01 85.3 

3 .3D 1.32 .20 43 4.23 85.2 

I .24 1.34 .20 46 7.47 84 .. 9 

.. 30 .94 .20 46 2.93 84.8 

.27 .92 .20 48 3.54 1.04 84.7 

REV 032 

1 .36 1.42 .21 33 3.81 96.2 

I 2 .27 1,.39 .21 37 5.59 86.4 

3 .42 1.72 .21 46 4.48 84.9 

.27 .89 .20 50 3.44 84 .. 5 

5 .27 1.34 .21 49 5.30 84.5 

6 .35 1.36 .21 52 3.71 84 .. 4 

7 .44 1.39 .21 53 3.01 84.3 

I REV 033 

.12 72 1.81 96 .. '2 

.12 72 1.90 99 .. <) 

REV 034 

I .20 18 1.92 Q6 .. 2 

.. 42 2 .. 06 .20 63 6.88 2.46 84 .. 6 

.30 1.96 .20 63 8.69 2.30 84 .. 7 

REV D36 

I 1 .57 2.12 .20 16 5.56 96.2 

2 .76 2.33 .20 16 6.47 92.2 

3 .53 1.90 .20 21 4 .. 41 90.8 

4 .54 1.98 .21 21 4.83 90.5 

5 .39 2.30 .21 25 10.86 89.4 

6 .42 2.29 .21 25 10.02 89.2 

.11 31 1.70 87 .. 8 

I .10 31 1.60 87.5 

REV D37 

1 .. 59 1.00 .21 18 1.56 2.00 Q6 .. 2 

2 .55 1.50 .21 18 2.70 1.85 91.5 

3 .40 1.00 .21 26 2.23 1.73 89.0 

I .45 1.23 .21 26 2.50 1.50 88.7 

.29 .95 .13 32 2.52 1.61 87.1 

.35 1.12 .21 34 2.92 2.12 86.6 

.47 1. 15 .21 36 2.22 86.3 

.50 1.66 .21 36 3.56 86.1 

y .29 .55 .21 39 1.97 1 .. 80 85.7 

10 034 .58 .21 39 1.72 1 .. QO 85.5 

I 11 .70 1.62 .21 80 2.56 2.15 92.8 

I 

I 

I Handle via Byeman 

~T 

A-25 

Controls Only - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 
~ 

I ~'!1~~~~a~e: 201~2~~.l£0..s103025 Handle via Byeman BCS 39739-65 Controls Only 

I 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I Ace. NO. DENSI TY DE NS !TY SUN ANGLE BRIGHTNESS CLOUD AL TlTUDE 

DM!N DMAX BASE + FOG (DEGREES) RANGE DMAX (NM) 

REV 038 

I .11 14 .94 96.2 

I 2 .11 14 1.06 92.8 

3 .72 .96 .21 19 1.29 1.94 91.2 

" .45 1.42 .21 21 3.04 1.55 90.5 

5 .42 1.30 .21 21 2.85 1.48 90.2 

6 .36 1.80 .21 24 5.77 1.82 89.7 

7 .36 1.52 .21 24 4.23 1.49 89.5 

8 .66 1.08 .21 26 1.55 1.38 88.9 

I 9 .50 1.03 .21 26 1.87 1.91 88.6 

10 .80 1.80 .21 27 2~79 2.16 88.2 

11 .21 35 2.16 86.4 

12 .13 35 Z.OI 86.2 

13 .38 1.50 .21 45 3.87 1.40 84.7 

14 .39 I.D2 .21 45 2.32 1.60 84.7 

15 .62 1.30 .21 47 2.0D 1.70 84.5 

I 16 .12 50 1.40 84 .. 3 

17 .12 52 1.60 84.2 

18 .12 54 1.60 84.2 

1 Q .12 54 1.6D 8492 

20 .ll 57 1.76 84 .. 3 

21 .34 1.33 .21 59 3.72 2.14 84.4 

21 .11 59 1.56 84 .. 4 

I 22 .43 .8D .21 60 1.72 2.18 84.5 

Z3 .43 .62 .21 61 1.40 2.34 84 .. 5 

24 .44 1.42 .22 62 3.11 2,32 84 .. 6 

25 .44 1.48 .22 62 3.31 2.40 84.7 

26 .12 78 1.80 90.0 

27 .80 1.20 .22 77 1.47 2.44 93.2 

I 28 .70 1.16 .22 77 1 .. 59 2 .. 44 93.7 

29 .63 1.60 .22 77 2.72 2.20 94.2 

REV D39 

1 .47 .86 .21 11 1.70 1.7(t 96.2 

2 .50 .88 .21 11 1.63 1.42 93 .. 5 

I 3 .12 28 1.48 88.2 

.ll 28 1.46 88.0 

.54 1.30 .22 30 2.24 2.15 87.5 

6 .32 1.55 .21 43 5 .. 02 85.0 

7 .30 1.54 .21 43 5.32 84.9 

8 .49 1.32 .22 44 2.53 1.53 84.8 

9 .28 l. 58 .22 49 6.26 84.4 

I 10 .32 1.54 .22 49 4.96 B4~ 4 

II .34 2.22 .21 51 11.22 2.25 84.2 

IZ .40 2.32 .21 52 11.00 2.26 84.2 

13 .36 2 .. 08 .22 53 8.34 1.78 84.2 

1', .30 1.80 .22 54 7'[0 2.08 84.2 

15 .25 2.31 .22 56 22.19 1.90 84 .. 2 

16 .25 2m 1'+ .22 56 16.55 2.20 84 .. 2 

I 17 .10 64 1.60 84.8 

18 .11 64 1.62 84.9 

ReV 040 

I .22 8 1.30 96.2 

2 .22 8 1.50 94.0 

I 3 .62 1.50 .22 16 2.47 1.96 92.2 

4 .44 1.32 .22 16 2.80 1.99 91.9 

5 .11 IS 1.53 91.5 

6 .11 18 1,32 91.2 

7 .. 52 1.1 2 .23 30 1.95 1.32 87 .. 5 

.48 1.52 .22 35 3.18 86 .. 4 

I 9 .59 1.52 .22 35 2.61 86.2 

10 .67 1.69 .23 39 2.87 85.6 

11 .65 1.90 .22 39 3.74 85 .. 4 

12 .26 2.08 .22 42 13.74 85.1 

13 .27 1.81 .21 42 S .82 85.0 

14 .40 1.10 .22 44 2.45 84 .. 7 

15 .48 1.23 .22 44 2.35 84.7 

I 16 .28 2.26 .22 46 15.56 1.76 84 .. 6 

17 .44 1.26 .22 54 2.63 84 .. 2 

17 .72 1.10 .14 54 1.41 84.2 

17 1.10 1..26 .22 54 1.17 84.2 

17 .27 .42 .11 54 1.43 84.2 

17 .73 1.62 .22 54 2.48 84.2 

17 .28 .34 .12 54 1.18 84.2 

I 17 .46 1.29 .22 54 2.60 84 .. 2 

17 .34 .. 52 .12 54 1.41 84.2 

17 .86 1.28 .22 54 1.49 84.2 

17 .28 1.48 .12 54 4.76 84.2 

17 .73 1 ~ 98 .22 54 3.81 84 .. 2 

I 

I 

I Handle via Byeman A-26 

Controls Only T~T - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 
~ 

I Approved for Release: 2018/09/11 C05103025 ~j,JJ::.J""".1".L:J.L - U.t"l.lV.1.1.J.1 .L Handle via Byeman 

BCS 39739-65 Controls Only 

I 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUAT ION 

I ACC. NO. DE"S 11 Y DENS ITY SUN ANGLE BR IGHTNESS CLOUD ALTITUOE 

D~, I N Dr-",AX BASE + FOG !DEGREES) RANGE DMAX ( NMJ 

REV 1)41 

I .22 .78 96 .. 2 

.22 ' .74 95.6 

.22 1.47 94.7 

.21 2.00 94.4 

.21 1.88 94 .. 0 

6 .56 1. 38 .21 14 2 .. 34 2.01 92.7 

7 .48 1 .. 16 .22 14 2.20 1.94 92~3 

I .12 15 1.36 91.7 

9 .64 1.72 .22 18 3.07 2~O3 9Lo 

10 .11 26 1.78 8B.7 

11 .11 26 1.84 88.5 

12 .22 28 2.40 88.2 

13 .22 27 2.32 88 .. 0 

I lit .54 1.24 .22 30 2.10 2.25 87 .. 5 

1" .11 32 1. 72 87.2 

I·, .11 32 1.84 87.0 

17 .56 1.'.,.0 .12 33 2030 2.30 86.7 

Ie .11 33 2 .. 00 86 .. 5 

19 .64 1.83 .22 37 3.47 85 .. 9 

20 .73 2 .. 04 .22 37 4.14 85. I 

I 21 .68 1.72 .22 38 2.93 85 .. 6 

22 .. 55 1 .. 48 .22 42 2.65 1.72 85 .. 0 

23 .58 1.48 .22 42 2.53 1.85 84.g 

2<. .30 1. 10 .22 44 3.41 84 .. 7 

25 .40 1.56 .22 44 3 .. 90 84 .. 6 

2A .itl 1 .. 44 .22 45 3.37 84.5 

27 .29 1. 22 .22 46 3.97 1.96 84 .. 4 

I 21> .11 52 1.65 84 .. 1 

29 .40 1.64 .22 54 4.26 84 .. 1 

30 .. 40 1 .. 61 .22 54 4.12 84.1 

31 .38 1.34 .13 59 2.94 1 .. 40 84.4 

32 .74 1.81 .22 59 3.03 1.57 84 .. 4 

33 .48 1.63 .22 68 3.58 2.28 86.1 

34 .. 60 1.62 .. 22 68 2.88 2.27 8603 

I 35 .43 1. 84 .22 72 5.01 2 .. 34 86.9 

36 .47 1.65 .22 72 3.74 2.34 87.1 

37 .54 1.60 .21 77 3.07 2.10 90.6 

3H .42 1.32 .22 77 2.91 2.15 91 .. 0 

3'1 .,t.6 1.65 .22 74 3.82 2 .. 34 q6 .. 9 

40 .{to 1.50 .22 74 3.66 2.37 97 .. 4 

41 .41 1.91 .22 74 5 .. 71 1.92 9B.l 

I 4/ .34 1.75 .22 74 5.85 2.22 98.5 

REV 042 

I .38 1.14 .22 2.68 96 .. 2 

.41 1.10 .22 4 2.40 1.18 96 .. 0 

I .. 3 f

t .. 80 .21 17 2.21 2.01 91.4 

.30 .g7 .22 17 2.54 2.11 91.1 

• ~>1 .83 .22 20 1.51 1 .. 80 90 .. 4 

.46 1.31 .23 20 2.66 2.02 90 .. 0 

i .38 .83 .23 22 1.99 1.95 Fl9 ~ i+ 

U .33 1.10 .23 23 3.07 1.80 89 .. 2 

.40 1.10 .23 25 2.45 1.57 88 .. 9 

I 10 .47 1.12 .23 25 2.16 1.63 H8 .. 6 

II .29 .75 .21 27 2.50 1.98 88.1 

Ii .41 1.11 .22 27 2.42 2.03 87.9 

13 .35 1.18 .23 29 3.09 87 .. l 

14 .53 1. 51 .22 30 2 .. 84 87.3 

15 .57 1 .. &0 .23 31 2.91 8LO 

16 .38 1.38 .24 33 3.41 86.7 

I 17 .49 1.52 .23 33 3.12 86.6 

Ie .48 1.19 .22 34 2.26 86.3 

19 .38 1.37 .22 35 3.38 86.2 

20 .49 1.45 .23 35 2.90 86 .. 0 

21 .44 1.42 .21 37 3.11 85.8 

22 .55 1.58 .22 39 2 .. 94 85.5 

23 .60 1..83 .22 39 3 .. 64 85.3 

I 24 .56 1.25 .22 40 2.04 2.18 85.2 

20 .34 .90 .23 42 2.46 1.98 85.0 

26 .39 1.04 .22 42 2.36 1.62 84.9 

27 .36 1 .. 01 .22 43 2.55 2.03 84 .. 8 

28 .33 1.13 .23 46 3016 84.5 

29 .35 1.15 .22 46 3.00 84 .. 5 

3D .90 1.50 .22 55 1.81 84.2 

I 31 .78 1.45 .22 55 1.95 84.2 

32 1.30 1.60 .22 64 1037 85.1 

3, .90 1.22 .13 64 1. 33 85.2 

3', .41 .95 .23 73 2.08 1.82 87.3 

3' .39 .82 .?? 73 1.91 2.05 87.6 

31 .33 1 .. 00 .23 78 2.80 2.20 89.6 

I 37 .40 1.11 .22 78 2.47 2.01 go .. o Jh .. .38 .95 .23 77 2.25 2 .. 14 90 .. 8 

3" .46 .94 .23 79 1 .. 86 1.98 93.6 

4ll .. 12 78 1 .. aA 95.1 

41 .12 78 1.87 95.6 

4.- .12 76 1.66 <}6 .. 2 

43 .. 12 76 1 .. 78 <)6 .. 7 

I 44 .::>0 1. ~e • .:3 75 3.26 2 .. ill 98 .. 0 

4', .40 L~l ... !3 75 3 .. 34 2.06 98 .. 6 

4 6 .90 1.68 .. 23 64 2.2D 1.00 105.7 

47 877 l .. :d .23 64 2.14 .. 86 106 .. 4 

I Handle via Byeman A-27 

Controls Only 

Approved for Release: 2018/09/11 C05103025 
I ~ve~!£r .5~I~~e.;. 2018(9.~/l1.f2:1 ~3025 Handle via Byeman 

BCS 39739-65 Controls Only 

PERFORMANCE EVALUATION TEAM 

I REPORT NO. 4022/65 

PHOTOGRAPHIC EVALUATION 

I ACC. NO. DE~JSITY DENSITY SUN ANGLE BRIGHTNeSS CLOUD A L T I TUDE 

OMIN Or-lAX BASE + FOG (DEGREES) RANGE DMAX I NM J 

I REV D43 

.22 3 1.28 96.2 

.22 3 .94 96.3 

.22 14 2.25 92.3 

.H .54 .22 16 1.61 2.13 91.5 

.. 36 .. 64 .22 16 1.72 2.15 91.3 

I .52 2 .. 24 .22 IB 7.50 2.0D 91.0 

.50 .84 .22 20 1.56 2.35 90 .. 4 

8 .21 .4; .14 20 1 .. 52 2.12 90.1 

9 .36 1.35 .22 22 3.54 B9.7 

J 0 .;2 1 .. 46 .22 22 4.57 89.5 

II .12 25 1.96 BB.A 

12 .12 25 1.97 88. It 

I 13 .68 1.12 .14 29 1.51 2.17 87.7 

14 1.05 1.45 .23 29 1.49 2.40 87. S 

IS .48 .78 .12 31 1.50 1.85 B7.3 

16 .43 .72 .12 31 1.55 1.97 87 .. 0 

17 .64 1.44 .22 33 2.27 2.3B 86 .. 7 

18 .62 1.40 .22 33 2.22 2.42 86 .. 5 

19 .57 1.42 .23 34 2.41 2.46 86.2 

I 2D .38 1.25 .22 42 2.98 2 .. 44 85.0 

21 .43 1.56 .22 42 3.67 2 .. 44 84 .. 9 

n .30 1.15 .22 48 3.57 1.42 84 .. 4 

23 .31 1.08 .22 48 3.23 .85 84.3 

24 .85 1.88 .22 52 2.89 B't .. 2 

20 .54 1.65 .13 52 3.02 84 .. 2 

26 .89 1 .. 75 .22 53 2.40 1.77 84 .. 2 

I n .11 61 .98 84.6 

26 .11 61 .95 84 .. 8 

29 .72 1.22 .22 69 1.64 2.22 86.1 

30 .90 I. /

t5 .22 69 1.71 2 .. 20 86 .. 3 

31 .. 't2 .82 .22 74 1.79 2.26 88.0 

3;. .48 .67 .22 74 1.34 2.17 88.3 

33 .40 1.68 .22 75 4.46 2.28 88.6 

I REV LJ44 

.43 1 .. 56 .22 6 3.67 96. ~ 

.24 1.90 .22 5 13.85 95 .. 2 

.81 1.00 .22 23 1.21 2.22 89.4 

I 4 .64 .86 .22 23 1.29 2 .. 08 89.1 

0 .34 .63 .22 52 1.82 2.00 84.1 

.40 .66 .22 52 1.55 2.20 84 .. 1 

KEV 1)47 

.21 .97 96 .. 2 

I .21 7 .88 94.0 

.,38 1.76 .21 23 5.15 88.9 

.60 1.72 .22 23 3.22 88 .. 6 

.10 36 1. 02 85.8 

.13 36 1.56 85.7 

.. 28 .60 .21 42 2.28 1.86 84.8 

.35 1.28 .21 48 3 .. 41 8 i t .. 1 

I 9 .28 1 .. 48 .21 50 5 .. 63 A4 .. 1 

10 .26 1.53 .21 52 1.05 84.1 

11 .31 1.50 .22 52 .4.93 84.1 

U .22 72 2 .. 06 87.2 

13 .22 72 1. 66 87.5 

14 .46 1.28 .22 77 2.58 2.20 91.1 

t s .36 1.58 .22 77 4.51 2.18 91 .. 4 

I REV D4S 

1 .13 21 2.05 96.2 

1 .23 21 2 .. 10 89.4 

1 .. 1'3 21 1 e 72 89 .. 4 

2 .22 25 1.52 88.3 

I .22 25 1.50 8801 

.33 .80 .22 35 2.29 1.. 43 86 .. 0 

.31 .79 .22 35 2.43 L.15 85.8 

.45 1.35 .. 21 40 2.83 85.1 

.55 1 .. 46 .22 40 2.59 85.0 

.65 1 .. 39 .22 43 2.13 84.6 

I .81 1.55 .22 'd 2.09 84.5 

.06 1.77 .22 44 3.57 84.5 

.32 1.56 .22 45 5.07 84.4 

.. 32 1.16 .20 52 3.36 2.00 84.1 

Rf. V [\1,';1 

I .22 68 2 .. 29 96 ~ 2 

.22 68 2 .. 27 103 .. Ii 

REV U,:>U 

.22 16 1..44 96. ;( 

.23 16 1.50 90.5 

I " 23 1.76 .!.:l 2'. 14 .. 20 1.86 88.3 

.23 1.70 .23 24 13.29 1 .. 87 88.1 

I Handle via Byeman A-28 

Controls Only 

Approved for Release: 2018/09/11 C051 03025 
I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

I 

~ 

~ 

'1~pp~ed for Release: 2018/09/11 C051 03025 t...I..L...I"",..L\,...L...I..I. - '-...A&JI..L~.L.LJ"".L 

BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

REV 052 

1 

RE:V 053 

1 

l{) 

!l 

12 

13 

14 

15 

ReV [)54 

1 

2 

3 

10 

11 

L 

13 

14 

l' 

16 

17 

18 

20 

21 

2, 

23 

24 

2, 

26 

27 

28 

2Y 

30 

31 

32 

33 

34 

3:' 

36 

37 

38 

39 

40 

REV 055 

Handle via Byeman 

Controls Only 

10 

11 

Jj 

14 

1 ~) 

lo 

17 

18 

19 

20 

21 

2 ~' 

PHUTOGRAPHIC EVALUATION 

DENSITY DENSITY SUN ANGLE BRIGHTNESS 

OMIN OMAX BASE -+ FOG (DEGREES) RANGf 

.37 

.38 

.48 

.56 

.54 

.94 

.88 

.. 55 

.55 

.49 

.86 

1 .. 09 

.46 

.49 

.80 

.46 

.59 

.86 

.86 

.77 

.41 

.47 

.49 

• ?8 

.33 

.42 

.45 

.49 

.56 

.49 

.32 

.40 

.40 

.. t+8 

.33 

.. 30 

.. 44 

.40 

.43 

.. l::!6 

.72 

.38 

.. 43 

.66 

.74 

.46 

.83 

.53 

.58 

2.16 

2.10 

.63 

1.34 

1.42 

1.16 

1.06 

1.30 

1.18 

1.10 

1.33 

1.36 

1.55 

1. 01 

1.04 

1.06 

1 .. 08 

1.36 

1.68 

1.84 

1.78 

1.20 

1.10 

1.12 

1.00 

1.32 

1.12 

.96 

.90 

.70 

1.18 

.98 

1.88 

1.72 

1.02 

1.15 

1 ~ 00 

1.86 

1.68 

1.37 

1. 12 

2.30 

2.08 

2.32 

.85 

1.88 

2.28 

1.38 

1.26 

1 .. .3 L• 

1. 22 

1.2() 

1.35 

1. 16 

~22 

.n 

.22 

.22 

.22 

.22 

.22 

.23 

.23 

.22 

.22 

.22 

.13 

.13 

.23 

.23 

.23 

.23 

.23 

.23 

.15 

.23 

.12 

.21 

.12 

.21 

.22 

.22 

.22 

.ll 

.11 

.11 

.22 

.21 

.21 

.21 

.n 

.22 

.11 

.11 

.11 

.22 

.22 

.21 

.22 

.. 21 

.21 

.11 

.11 

.11 

.11 

.11 

.22 

.21 

.21 

.21 

.21 

.21 

.22 

.21 

.21 

.22 

.13 

.13 

.22 

.22 

~ 2 2 

.22 

.22 

.22 

.13 

622 

.22 

.22 

• (' 2 

.22 

.22 

.22 

.22 

.;:: 2 

.22 

.;- 2 

.n 

• "2 

14 

14 

16 

20 

20 

23 

23 

18 

17 

25 

25 

25 

41 

41 

77 

17 

75 

75 

69 

69 

61 

61 

12 

12 

13 

21 

21 

23 

23 

25 

26 

26 

36 

36 

38 

39 

39 

41 

43 

43 

44 

46 

46 

47 

48 

48 

51 

53 

53 

55 

57 

58 

59 

76 

76 

·78 

78 

79 

78 

78 

77 

77 

11 

11 

31 

33 

33 

43 

43 

44 

46 

48 

48 

51 

53 

54 

54 

55 

58 

58 

61 

61 

66 

66 

~ET-GAMBIT 

13.60 

10.47 

6.09 

7.17 

12.10 

4.10 

4.04 

6.15 

5.58 

1.25 

1.59 

1 .. 39 

2.29 

1.96 

1.63 

2.33 

1.67 

1.57 

1.62 

2,J9 

2 .. 20 

2.01 

1.96 

1.70 

3.97 

4.28 

4.81 

4 .. 15 

1.50 

(' .. 64 

2.06 

2.86 

2.80 

2.27 

2.71 

2.10 

3 .. ~d 

2.62 

2.83 

1.29 

8 .. 16 

5.20 

17.28 

3.97 

13.47 

16.1 1 

6 .. 03 

4.47 

'+~03 

2.74 

2 .. 38 

3013 

2.59 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

Controls Only 

CLOUD 

OMAX 

1.76 

1 .. 76 

1.97 

2.06 

1.98 

1.14 

1.04 

2.20 

2 .. 20 

1.76 

1.68 

1.60 

1.'15 

1.20 

2 .. 00 

2.03 

1 d8 

1 .. 43 

1. ~";6 

2 .. 40 

2 .32 

L93 

2 .. 30 

2.16 

2. 3ft 

2.34 

1. 84 

1.76 

2 .. 24 

2.25 

2 .. 30 

1..97 

7 .. 00 

2.08 

1.1:18 

? .. 28 

2.30 

2.25 

2 .. 38 

2.32 

?38 

ALTITUOE 

{NM J 

')1.8 

9 1.5 

913 ~O 

1(13.1 

103 .. 7 

109 .. 4 

110 .. 0 

94.9 

A-29 
I nAp~el!. ~ ... R~~a1e: 20~~0.?DLS2~ 03025 Handle via Byeman 

Controls Only 

BCS 39739-65 

I PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

I PHOTOGRAPHlC EVALUATION 

Ace. NO. oENSl TV DENS I TY SUN ANGLE 8R I GHTNESS CLOUD ALTITUDE 

OMIN Ofo1AX BASE + FOG (DEGREES) RANGE DMAX (NM) 

I REV 056 

I .56 1010 .22 1.77 1.56 96.2 

2 .65 1.05 .21 1.52 .70 93.0 

3 .22 14 1.86 90.9 

.48 1.08 .23 16 2.04 1.80 90.3 

I .44 1.70 .22 16 4.20 1.93 90.1 

.22 18 1.82 89 .. 7 

.22 17 1.70 89.5 

8 1.00 1.40 .22 28 1.48 86.9 

9 .52 1.29 .22 30 2.30 86.5 

10 .31 1.54 .22 30 5014 86.4 

II .51 .98 .22 32 1.75 85.9 

I 12 .51 1.42 .21 34 2.69 85.6 

!3 .86 2.03 .22 34 3.52 85.5 

14 .43 1.80 .22 37 't.SO 85.2 

15 .62 1.90 .22 37 3 .. 87 85.1 

16 .62 1 .. itS .22 40 2.42 84 .. 7 

17 .. LI6 I.! 7 .22 40 2.31 84 .. 6 

18 .40 1.05 .22 41 2.33 84 .. 5 

I 19 .13 45 1.73 84 .. 2 

20 .13 45 1.82 84 .. 2 

21 .48 1.09 .22 47 2.06 1.48 84.1 

22 .50 2.00 .22 49 5.38 2 .. 02 84 .. 0 

23 .42 2.26 .22 50 9.52 84 .. 0 

24 .38 1.38 .22 51 3.41 84 .. 0 

25 .56 1.56 .22 52 2.82 84 el 

I REV 05·' I .22 4 1.10 96.2 

2 .30 .40 .22 4 1.39 .80 93.8 

3 .22 I'. 1.24 90.8 

I 4 .22 14 I.! 3 90.5 

5 .12 17 1.02 A9 .. 9 

6 .14 17 1.24 89 .. 6 

7 .40 1.16 .22 17 2.59 2.32 89 .. 4 

B .56 ) .28 .22 27 2.10 2.03 87.0 

9 .56 .72 .22 28 1.20 2.16 86.8 

10 .12 29 1.64 86 .. 6 

I II .53 .90 .22 30 1.56 2.32 86 .. 3 

12 .55 .87 .22 32 1.45 2.16 86 .. 0 

13 .66 .76 .21 32 1.12 2.16 85.9 

14 .26 .46 .12 34 1.60 1.71 85.7 

15 .86 1.20 .22 34 1.37 2.38 85.5 

16 .79 .99 .22 36 1.22 2.33 85.2 

17 .12 36 2.10 85.1 

I 18 .12 38 1.88 84.8 

19 .36 1 e 59 e 21 45 4.57 1.71 84 .. 2 

20 .32 1.60 .21 45 5.30 2.10 84.1 

21 .52 2.14 .22 59 6.31 84.5 

22 .59 2.12 .22 59 5.43 84 .. 6 

I REV 058 

I .50 2.20 .22 1I 7.29 1.96 96 .. 2 

2 .47 2.36 .22 11 10.53 1.83 91.4 

3 .38 .. so .22 20 1.93 2.23 88 .. 6 

.33 1.24 .22 22 3.50 2.33 88 .. 2 

.35 1.90 .22 22 6.73 2.32 88.0 

.32 1 .. 80 .22 23 6.62 2.16 8·' .. 8 

I .22 26 2.23 87.2 

.22 26 2.14 87.1 

9 .34 1.32 .21 29 3.68 1.15 86.5 

10 .38 1.66 .22 29 4 .. 61 .. 76 86 .. 3 

11 .34 1 .. 3'. .22 31 3.76 86.0 

12 .. 't3 1.26 .22 31 2.68 85.9 

13 .38 1.03 .22 34 2.42 85.5 

I 14 .48 1.25 .22 34 2 .. 40 85 .. 4 

15 .48 1 .. 6'. .22 36 3.62 8501 

16 .46 1.66 .22 36 3.86 85.0 

17 .51 1 .. 51 .. 22 40 2 .. 96 8'+ .. 7 

18 0"/3 1.70 .22 40 2.71 84 .. 6 

19 .84 1..46 .22 54 1.84 1.76 84 .. 1 

I 20 .78 1.53 .22 54 2.12 2.06 84.1 

REV D~9 

.24 1.18 96.2 

.23 3 .98 94.0 

.26 1.27 .23 31 5.37 2 .. 39 86.0 

I .35 1.30 .23 32 3 .. 48 1.83 85 .. 8 

.44 1.11 .23 33 2.28 85.6 

.52 1.30 .23 33 2.33 2.20 85 .. 4 

.23 35 2.22 85.2 

I 

I Handle via Byeman 

Controls Only T~T GAMBIT A-30 - Approved for Release: 2018/09/11 C051 03025 
I 

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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

ACC. NO. fJENSITY 

Of-lIN DMAX 

REV 063 

1 

.62 .84 

1 .. 09 1036 

.26 .90 

.25 1.02 

.34 1.39 

.38 1 .. 49 

REV 064 

1 .42 .63 

2 .38 1.58 

.28 .36 

.29 .36 

.42 1.40 

.43 1.44 

8 .30 1.08 

9 .37 1.15 

10 .33 1 .. 36 

-

PHOTOGRAPHIC EVALUATION 

DENSITY SUN ANGLE 

ESASE + FOG (DEGREES) 

.22 

.22 26 

.13 26 

.22 26 

.22 39 

.22 44 

.22 60 

.22 60 

.23 13 

.23 17 .14 17 

.23 17 

.23 24 

.23 32 

.23 32 

.22 36 

.23 36 

.23 45 

.22 45 

.23 52 

Handle via Byeman 

Controls Only T~ET - GAMBIT 

BRIGHTNESS 

RANGE 

1.28 

1.31 

3.79 

4.66 

3.96 

3.83 

1.44 

4.21 

1.39 

1.28 

3 .. 17 

3.24 

3.34 

2.80 

3.97 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

Controls Only 

CLOUO ALTITUOE 

DMAX I NM I 

.73 96.2 

1.60 86.7 

.79 86.7 

1.36 86 .. 7 

.86 84.5 

1.02 84.1 

2.28 84 .. B 

2.30 84.9 

1.22 96 .. 2 

1.40 89.0 

1.10 89.0 

1" 38 89.0 

1.70 81 .. 0 

.44 85 .. 6 

.47 85.5 

84 .. 9 

84.,8 

.90 84.1 

.70 84.0 

1.67 84.0 

A-31 
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I ~!:..o~ed ~~R~~a~s~ ~018/0@!:11_£Q.~ Q.3Q25 Handle via Byeman 

Controls Only 

BCS 39739-65 

I PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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BCS 39739- 65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

Handle via Byeman 

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PHOTOGRAPHS NO. 14 & NO. 15 

These two photographs provide a comparison 

of duplicate photography obtained of radio towers 

and bridge at Milwaukee, Wisconsin, on Missions 

4017 and 4022. 

PHOTOGRAPH NO. 14 

(Mission 4017) 

Rev D31 

Altitude: 87.55 NM 

Scale: 1:84,670 

20X 

Frame 003 

Obliquity: + 10. 0° 

Strip 

PHOTOGRAPH NO. 15 

Rev D31 

Altitude: 85.4 NM 

Scale: 1:89,200 

20X 

Frame 001 

Obliquity: -24.4° 

Strip 

~T-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

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B-1 
PHOTOGRAPH 14 

B-2 

Tnn ~ _ ~II. l\/fOYT 

Approved for Release: 2018/09/11 C05103025 BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

~-GAMBIT 

Approved for Release: 2018/09/11 C05103025 

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Approved for Release: 2018/09/11 C05103025 

BCS 39739~65 ~RET - GAMBIT 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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Approved for Release: 2018/09/11 C05103025 

PHOTOGRAPH 15 

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PHOTOGRAPHS NO. 16 & NO. 17 

These two photographs provide a comparison 

of duplicate photography obtained of a gas 

storage tank in Chicago, illinois 

PHOTOGRAPH NO. 16 

(Mission 4017) 

Rev D31 

Altitude: 87. 3 NM 

Scale: 1 :92,300 

40X 

Frame 004 

Obliquity: 26.6° 

Strip 

PHOTOGRAPH NO. 17 

Rev D31 

Altitude: 85.3 NM 

Scale: 1:86,100 

40X 

Frame 003 

Obliquity: -13. 0° 

Stereo 

~-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

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B-4 
--- --~ ~ •• ,~y~ 

Appr~ed for Release: 2018/09/11 C05103025 BCS 39739-65 

PERFORMANCE EVALUATION TEAM I 

REPORT NO. 

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PHOTOGRAPH 16 

Approved for Release: 2018/.::..09:.:./..:..11.:....::::.C.:::.:05:::..:1~0.::..30::::.::2:.::5:- _____________ • 
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Approved for Release: 2018/09/11 C05103025 

BCS 39739-65 ~T-GAMBIT 

PERFORMANCE EVALUATION TEAM 

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Approved for Release: 2018/09/11 C05103025 

PHOTOGRAPH 17 

B-6 
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BCS 39739-65 

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PHOTOGRAPH NO. 18 

Football stadium with game in progress -

Chicago, TIL 

Rev D31 

Altitude: 85.2 NM 

Scale: 1:85,900 

20X 

Frame 003 

Obliquity: -13.0° 

Stereo 

T()P SECRE'J!-- GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

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B-7 
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BCS 39739-65 Approved for Release: 2018/09/11 C05103025 ~.l\...J..:.J.l - UClI.J. • .I.J...J'.J..l 

PERFORMANCE EVALUATION TEAM 

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TOP SECHE'f GAMBIT 

Approved for Release: 2018/09/11 C05103025 

PHOTOGRAPH 18 

B-8 
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PHOTOGRAPH NO. 19 

Midway Airport, Chicago, lllinois 

Rev D31 

Altitude: 85.3 NM 

Scale: 1:86,100 

lOX 

Frame 002 

Obliquity: -13.0° 

Stereo 

TOP SEC~ET - GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

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B-9 
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IBCS 39739-65 

Approved for Release: 2018/09/11 C05103025 

~.K.td· - UAMtll'!' 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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Approved for Release: 2018/09/11 C05103025 

PHOTOGRAPH 19 

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PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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PHOTOGRAPH NO. 20 

Hangar buildings, Lowry AF Base, Colorado 

Rev D48 

Altitude: 84.4 NM 

Scale: 1:80,500 

20X 

Frame 011 

Obliquity: + 6. 0° 

Strip 

~T-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

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B-ll 
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Bes 39739-65 Approved for Release: 2018/09/11 C05103025 ~\"'.c\,j:: .. J. - UfilV1DJ. J. 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

~-GAMBIT 

Approved for Release: 2018/09/11 C05103025 

PHOTOGRAPH 20 

B-12 
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BCS 39739-65 

PERFORMANCE EVALUATION TEAM 

REPORT NO. 4022/65 

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PHOTOGRAPH NO. 21 

Drive-in Theatre at Phenix City, Alabama 

Note Speaker Stands 

Rev D47 

Altitude: 84. 1 NM 

Scale: 1:87,907 

Frame 010 

40X 

Obliquity: -19.7° 

strip 

~ET-GAMBIT 

Approved for Release: 2018/09/11 C051 03025 

Handle via Byeman 

Controls Only 

B-13 
Approved for Release" 2 

BCS 39739-

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~RICT - ~ .••• ~!!,!09111 C05103025 

PERFORMANCE EVALUATION TEAM 

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Approved for Release: 2018/09/11 C05103025 

PHOTOGRAPH 21 

B-