CAMERA INFORMATION FOR MISSION 1001-1

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP78B04558A000600120015-7
Release Decision: 
RIPPUB
Original Classification: 
T
Document Page Count: 
10
Document Creation Date: 
December 28, 2016
Document Release Date: 
April 23, 2008
Sequence Number: 
15
Case Number: 
Publication Date: 
September 1, 1963
Content Type: 
CABLE
File: 
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PDF icon CIA-RDP78B04558A000600120015-7.pdf291.6 KB
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Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 T-n P S E C R E T S 311528Z OUT?51772 25X1 HFS CJS SUBJECT: CAMERA INFORMATION FOR MISSION 1001"19 A. THIS PHOTOGRAPHY INVOLVES THE _S OF EIGHT CAMERAS: TWO MAIN CAMERAS, FOUR HORIZON CAMERAS, STELLAR CAMERA AND AN INDEX CAMERA. (NOTE: STELLAR/INDEX DATA FOR 1001.2 INCLUDED). Be OPERATIONAL FOCAL LENGTHS FWD UNIT AFT UNIT 1 (1) MAIN LENS 609.120 MM 609.630 MM (2) PORT HORIZON LENS 88.96 MM 89.12 MM (3) STARBOARD HORIZON LENS 89.90 MM 89.10 MM (4) STELLAR CAMERA (1) 83.84 MM (2) 83.67 MM (5) INDEX CAMERA (1) 38.40 MM (2) 38.42 MM DEFINITION: "OPERATIONAL FOCAL LENGTH" IS DEFINED AS THE DISTANCE FROM THE MAIN LENS NODAL POINT TO THE FILM SURFACE AS MEASURED ON THE LENS BENCH, AND THE DATA REDUCED FOR A FACUUM CONDITION. (OPERATIONAL FOCAL LENGTH IS EQUIVALENT FOCAL LENGTH CORRECTED FOR ENVIRONMENT,.) Co LENS DISTORTION (PIN CUSHION) FWD UNIT AFT UNIT (1) MAIN LENS Declassification Review by NGA/DoD TOP SECRET TOPS1 Exc{nead is fl automaii [?~wn;rwUin, anu tassttun Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 ? Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 S -2- i- 3 DEGREES .003 lllM! .002 MM 2 DEGREES .''MM .001 MM 1 DEGREES .001 MM .000 MM 0 DEGREE .000 MM .000 MM 359 DEGREES NOT AVAILABLE NOT AVAILABLE 358 DEGREES NOT AVAILABLE NOT AVAILABLE 357 DEGREES NOT AVAILABLE NOT AVAILABLE (2) PORT HORIZON CAMERA (RADIAL DISTORTION) 10 DEGREES .021 MM .003 MM 20 DEGREES 9068 MM .042 MM (TANGENTIAL DISTORTION) MAXIMUM VECTOR .009 MM .009 MM (3) STARBOARD HORIZON CAMERA (RADIAL DISTORTION) 10 DEGREES .006 MM .015 MM 20 DEGREES .044 MM .062 MM (TANGENTIALHDISTORTION) MAXIMUM VECTOR .006 MM .000 MM DEPRESSION ANGLES OF HORIZON CAMERAS RELATIVE TO 1 1 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 ? NOMINAL MAIN CAMERA. (1) FWD UNIT A. PORT HORIZON CAMERA - 14 DECREES 49' 04" Be STARBOARD HORIZON CAMERA - 14 DEGREES 26' 23" (2) AFT UNIT A. PORT HORIZON CAMERA - 14 DEGREES 17' 55Z Be STARBOARD HORIZON CAMERA - 14 DEGREES 57' 94" E. FILTER AND EXPOSURE DATA (1) MAIN CAMERAS FWD UNIT AFT UNIT FILTER WRATTEN 21 WRATTEN 21 APERTURE F 3.5 F 3.5 SLIT WIDTH .200 INCH .tee INCH (2) PORT AND STARBOARD HORIZON CAMERAS FILTER WRATTEN 25 WRATTEN 25 APERTURE F 6.8 F 6.8 EXPOSURE 1/100 SEC 1/ 100 SEC (3) STELLAR CAMERAS Cl) AND (2) FILTER NONE APERTURE F 1.9 EXPOSURE 2 SEC (4) INDEX CAMERAS (1) AND (2) 1 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 ? FILTER WRATTEN 21 APERTURE F 4.5 EXPOSURE 1/580 SEC F. RESOLUTION CAPABILITIES Cl) MAIN LENS 1 A. B. FVD UNIT - 179.2 (L/MM AVID) AFT UNIT - 191.2 (L/MM AVG) (2) PORT HORIZON CAMERA A. B. FWD UNIT - 35.8 (L/MM AVG) AFT UNIT - 35.4 (L/MM AVG) (3) STARBOARD HORIZON CAMERA A. FWD UNIT - 36.2 CL/MM AVG) B. AFT UNIT - 37.6 (L/MM AVG) C4) INDEX CAMERA (1) 81.46 (L/MM AWAR) (5) INDEX CAMERA (2) 74.982 (L/MM AVAR) G. TIMING MARKS FREQUENCY MARKS VILL APPEAR ON THE FILM. RATE OF TIMING MARKS VILL BE 289 CYCLES PER SECOND. H. FILM DATA 1. MAIN CAMERAS - SO 132 2. HORIZON CAMERAS - SO 132 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 3.H STELLAR CAMERAS 1 AND 2 ? SO 102 4.. INDEX CAMERAS 1 AND 2 ? SO 130 I. CALIBRATED ANGLES OF CAMERAS to CALIBRATED CONVERGENT ANGLE OF MAIN CAMERAS ? 29 DEGREES 53.7 MINUTES 2. CALIBRATED ANGLE BETWEEN FRAMING AND STELLAR CAMERAS - MDT AVAILABLE 3. STELLAR ? I (.LOC. OF P.P.) 1. X EQUALS .000 MM 2. Y EQUALS MINUS .020 MM STELLAR ? 2 1. X EQUALS PLUS .0A8 MM 2. Y EQUALS MINUS .064 MM NOTE: VIEWING POSITIVE, EMULSION UPS COORDINATE SYSTEM IS DEFINED AS PLUS "Y" IN DIRECTION OF FLIGHT AND PLUS "X" TO THE LEFT AND PERPENDICULAR TO LINE OF FLIGHT. 4. INDEX - 1 (LOC. OF P.P.) X EQUALS PLUS .014 MM 2. Y EQUALS PLUS .0"6 MM INDEX - 2 1. X EQUALS MINUS .015 MM Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 6 2, Y EQUALS PLUS .021 MM NOTE: VIEWING POSITIVE, EMULSION UP9 PLUS "X" IS IN DIRECTION OF FLIGHT AND MINUS "Y" TO THE RIGHT AND PERPENDICULAR TO DIRECTION OF FLIGHT. J. IMAGE NOTION COMPENSATION DATA FMC PROGRAMMER REFERENCE LEVEL (1) GROUND ANGULAR VELOCITY (RAD/SEC) .0301 PASSES: IA1, 1A2, 1D1, 2A1, 3A1, 3D1, 302, 501, 6019 602 (2) GROUND ANGULAR VELOCITY (RAD/SEC) .0312 PASSES: 7D1, 702, 801, 9D1, 902, 16A1, 1701, 2101, 22D1, 2202, 22D3, 23D1, 24D1, 33A1, 33A2, 34A 1, 36D19 370 1, 38D 1, 39D2, 40D 1, 4802, 44A 1, 46A 1, 48A1, 490 1, 58A19 51A 1, 520 1, 5019 55D 1, 5601, 6401, 39D I FMC PROGRAMMER AMPLITUDE LEVEL GROUND ANGULAR VELOCITY (RAD/SEC) .0118 PASSES: USED FOR ALL PASSES NOTE I: SEE REMARKS (PARA L) K. PROGRAM TIME DATA PASS CAMERA ON TIME PROGRAM ON TIME PROGRAM 1 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 ? 7-- ? (ZEBRA TINE) UP RAMP DURATION DAY HOUR NIN (SEC) (SEC) IA I 25 01 41 667 142 1A2 25 01 47 1001 153 1D1 25 01 53 1355 130 2A1 25 03 13 724 125 3A I 25 04 42 608 261 3D1 25 04 53 1298 153 3D2 25 04 58 1601 172 5D1 25 08 01 1708 244 6D1 25 09 31 1718 170 6D2 25 09 36 2035 192 7D1 25 11 01 1630 120 7D2 25 11 04 1795 179 8D1 25 12 31 1730 222 9D1 25 14 03 1792 171 902 25 14 09 2171 100 16A1 26 00 21 861 143 1701 26 02 04 1599 160 2101 26 08 11 1886 120 22D1 26 09 36 1544 138 22D2 26 09 40 1811 203 ^ Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 22D3 26 09 44 23D1 26 11 11 24D1 26 12 45 33A I 27 02 02 33A2 27 02 06 34A1 27 03 32 36DI 27 06 53 "7D1 27 08 20 38D1 27 09 51 39D1 27 11 21 39D2 27 11 24 40D1 27 12 51 40D2 27 12 55 44A1 27 18 41 46AI 27 21 39 48A 1 28 00 39 49D I 28 02 23 50A1 28 03 40 51A1 28 05 16 52D1 28 07 02 54D1 28 10 01 2055 1881 1991 9 63 1200 931 20S6 1880 1892 1853 2033 1837 2080 1115 915 904 1691 845 1229 2115 2027 ? 1 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 55D1 28 11 30 1897 265 56D1 28 13 00 1881 377 64D1 29 61 01 1684 112 NOTE 2s DATA IS THE SAME FOR BOTH THE MASTER AND SLAVE UNITS 1.. REMARKS THE RAMP FOR THIS MISSION IS A MODIFIED SINUSOIDAL CURVE OF 4800 SECONDS DURATION AND SYMMETRICAL ABOUT THE 2400 SECOND MARK. IN ORDER TO PLOT THIS CURVE WE MUST EQUATE THE 4808 SECONDS TO ITS EQUIVALENT IN DEGREES 210. THE CURVE REPRESENTS GROUND ANGULAR VELOCITY (RADIANS/SECONDS) VS TIME (DEGREES). THE CURVE IS MADE UP OF THREE SECTIONS EACH HAVING ITS UNIQUE EQUATION. FROM 0 DEGREES TO 60 DEGREES, THE EQUATION OF THE CURVE IS K SIN (THREE HALFS X - 90 DEGREES). THE SEGMENT FROM 60 DEGREES TO 150 DEGREES HAS THE EQUATION K SIN (2 X - 120 DEGREES) AND THE LAST SEGMENT FROM 150 DEGREES TO 210 DEGREES IS DEFINED BY K SIN ( THREE HALFS X - 45 DEGREES). THE TWO VARIABLES X AND K ARE GIVEN. "X" IS THE TIME (DEGREES) OR SCALE ON THE ABSCISSA AND K IS GIVEN IN THIS CABLE AS A GROUND ANGULAR VELOCITY VALUE. THE ORDINATE OF THE GRAPH RANGES FROM THE "REFERENCE LEVEL" VALUE (GIVEN) IN GROUND ANGULAR VELOCITY (RADIANS/SECOND) TO PLUS AND MINUS THE K VALUE WHICH REPRESENTS THE AMPLITUDE OF THE CURVE. WITH THIS CURVE PLOTTED AND 1 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7 0 -/?- ? THE TIME UP THE RAMP PROVIDED FOR EACH PHOTOGRAPHIC OPERATION (PASS OR SEGMENTS THEREOF) THE CAMERA RATES FOR THAT PASS CAN BE FOUND. THE FOLLOWING CONVERSION FACTORS WILL ALLOW ONE TO GO FROM GROUND ANGULAR VELOCITY TO CYCLE PERIOD TO SCAN VELOCITY TO IMAGE MOTION COMPENSATION VELOCITY. 1. CYCLE PERIOD (SECONDS) EQUALS THE RECIPROCAL OF THE GROUND ANGULAR VELOCITY (RADIUS PER SECOND) (11.0574) 2. SCAN VELOCITY (INCHES PER SECOND) EQUALS (24) (6.2834) DIVIDED BY THE CYCLE PERIOD (SECONDS) 3. INC VELOCITY (INC/SEC) CENTER OF FORMAT EQUALS 22.3921 (GROUND ANGULAR VELOCITY RAD/SEC) M. TIME CORRELATION (READINGS IN MILLISECONDS) PASS SYSTEM TIME CLOCK TIME DIFFERENCE 09 49386.840 308451, 664 25 50067.848 395532.680 PLUS .008 47 84752, 940 516617.794 PLUS .022 56H 45760.338 27154.282 PLUS .001 TOPS E C R E T END OF MESSAGE 1 L.- Approved For Release 2008/04/23: CIA-RDP78BO4558A000600120015-7