Source Code
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These source-code files were obtained by digitally photographing
an Artemis 72 (Apollo 15-17 Command Module) program listing from a private
collection and then
modifying pre-existing Comanche 55 (Apollo 11) source files to
incorporate changes. Photography was by Ron Burkey, and transcription
was performed by a team of volunteers. Note that the page images
presented online are of reduced quality, and that additional images
may be available. Report any conversion errors or legibility
problems in page images to info@sandroid.org.
Notations on the program listing read, in part:GAP: ASSEMBLE REVISION 072 OF AGC PROGRAM ARTEMIS BY NASA 2021114-011 11:40 FEB. 26, 1971Note that the date is the date of the printout, not the date of the program revision. |
037266,000002: ## Copyright: Public domain.
037267,000003: ## Filename: ENTRY_LEXICON.agc
037268,000004: ## Purpose: Part of the source code for Artemis (i.e., Colossus 3),
037269,000005: ## build 072. This is for the Command Module's (CM)
037270,000006: ## Apollo Guidance Computer (AGC), for
037271,000007: ## Apollo 15-17.
037272,000008: ## Assembler: yaYUL
037273,000009: ## Contact: Jim Lawton <jim DOT lawton AT gmail DOT com>
037274,000010: ## Website: www.ibiblio.org/apollo/index.html
037275,000011: ## Page Scans: www.ibiblio.org/apollo/ScansForConversion/Artemis072/
037276,000012: ## Mod history: 2009-08-11 JL Adapted from corresponding Comanche 055 file.
037277,000013: ## 2010-02-20 RSB Un-##'d this header.
037278,000014: ## 2017-01-22 RSB Proofed comment text by diff'ing vs Comanche 55
037279,000015: ## and corrected errors found.
037280,000016:
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Page 842 |
037282,000018:
037283,000019: # VARIABLE DESCRIPTION MAXIMUM VALUE * COMPUTER NAME
037284,000020: # -------- ----------- ------- ----- -------- ----
037285,000021: # -
037286,000022: # URT0 INITIAL TARGET VECTOR 2 (UNIT VECTOR) = RTINIT
037287,000023: # -
037288,000024: # UZ UNIT VECTOR NORTH 1 = UNITW
037289,000025: # -
037290,000026: # V VELOCITY VECTOR 2 VSAT = VEL
037291,000027: # -
037292,000028: # R POSITION VECTOR 2 EXP 29 METERS = RN
037293,000029: # -
037294,000030: # VI INERTIAL VELOCITY 128 M/CENTISEC = VN
037295,000031: # -
037296,000032: # RTE VECTOR EAST AT INITIAL TARGET 2 = RTEAST
037297,000033: # -
037298,000034: # UTR NORMAL TO RTE AND UZ 2 = RTNORM
037299,000035: # -
037300,000036: # URT TARGET VECTOR 2 = RT
037301,000037: # -
037302,000038: # UNI UNIT NORMAL TO TRAJECTORY PLANE 2
037303,000039: # -
037304,000040: # DELV INTEGRATED ACCEL. FROM PIPAS 5.85 16384 CM/S
037305,000041: # -
037306,000042: # G GRAVITY VECTOR 128 M/CENTISEC = GDT/2
037307,000043:
037308,000044: # A0 INITIAL DRAG FOR UPCONTRL 805 FPSS FPSS=FT/SEC/SEC
037309,000045: # AHOOKDV TERM IN GAMMAL CALC. = AHOOK DVL 8
037310,000046: # A1 DRAG VALUE IN FACTOR CALCULATION 805 FPSS
037311,000047: # ALP CONST FOR UPCONTRL 1
037312,000048: # ASKEP KEPLER RANGE 21600 NM NM = NAUTICAL MILE
037313,000049: # ASP1 FINAL PHASE RANGE 21600 NM
037314,000050: # ASPUP UP-RANGE 21600 NM
037315,000051: # ASP3 GAMMA CORRECTION 21600 NM
037316,000052: # ASPDWN RANGE DOWN TO PULL-UP 21600 NM
037317,000053: # ASP PREDICTED RANGE 21600 NM NOT STORED
037318,000054: # COSG COSINE(GAMMAL) 2 = COSG/2
037319,000055: # C/D0 RECIPROCAL DRAG, -4/D0 B-8 64/FPSS AGC ONLY
037320,000056: # D TOTAL ACCELERATION 805 FPSS
037321,000057: # D0 CONTROLLED CONSTANT D 805 FPSS
037322,000058: # DHOOK TERM IN GAMMAL COMPUTATION 805 FPSS
037323,000059: # DIFF THETNM-ASP (RANGE DIFFERENCE) 21600 NM
037324,000060: # DIFFOLD PREVIOUS VALUE OF DIFF 21600 NM
037325,000061: # DLEWD CHANGE IN LEWD 1
037326,000062: # DR REFERENCE DRAG FOR DOWNCONTROL 805 FPSS NOT STORED
037327,000063: # DREFR( ) REFERENCE DRAG (FINAL PHASE TABLE) 805 FPSS NOT SAVED
037328,000064: # DVL VS1-VL 2 VSAT
037329,000065: # E ECCENTRICITY 4 NOT STORED
037330,000066: # F1( ) DRANGE/D DRAG (FINAL PHASE TABLE) 2700/805 = FX +5
037331,000067: # F2( ) DRANGE/D RDOT (FINAL PHASE TABLE) 2700/2VS NM/FPS = FX +4 /8
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037333,000069: # F3( ) DRANGE/D (L/D) (FINAL PHASE TABLE) 2700 NM = FX
037334,000070: # * MAXIMUM VALUE DENOTES UNSCALED
037335,000071: # VARIABLE VALUE WHEN SCALED
037336,000072: # FIGURE 7.0-2 COMPUTER VARIABLES VARIABLE HAS MAXIMUM VALUE OF ONE.
037337,000073:
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037339,000075:
037340,000076: # VARIABLE DESCRIPTION MAXIMUM VALUE COMPUTER NAME
037341,000077: # -------- ----------- ------- ----- -------- ----
037342,000078:
037343,000079: # FACT1 CONST FOR UPCONTRL 2 VSAT
037344,000080: # FACT2 CONST FOR UPCONTRL 1/805 FPSS
037345,000081: # FACTOR USED IN UPCONTRL 1
037346,000082: # GAMMAL FLIGHT PATH ANGLE AT VL 1 RADIAN
037347,000083: # GAMMAL1 SIMPLE FORM OF GAMMAL 1 RADIAN
037348,000084: # HEADSUP INDICATOR FOR INITIAL ROLL 1
037349,000085: # KA DRAG TO LIFT UP IF DOWN 805 FPSS = KAT
037350,000086: # KLAT LATERAL SWITCH GAIN 1 (NOM = .0125)
037351,000087: # K2ROLL INDICATOR FOR ROLL SWITCH
037352,000088: # LAD MAX L/D (MIN ACTUAL VEHICLE L/D) 1
037353,000089: # LADPAD NOMINAL VEHICLE L/D, SP PAD LOAD 1 (NOM = 0.3)
037354,000090: # LATANG LATERAL RANGE 4 RADIANS
037355,000091: # LAT(SPL) GEODETIC LATITUDE OF TARGET 1 REVOLUTION
037356,000092: # LNG(SPL) LONGITUDE OF TARGET 1 REVOLUTION
037357,000093: # LEQ EXCESS C.F. OVER GRAV=(VSQ-1)GS 128.8 FPSS
037358,000094: # LEWD UPCONTROL REFERENCE L/D 1
037359,000095: # LOD FINAL PHASE L/D 1 (NOM = 0.18)
037360,000096: # LODPAD FINAL PHASE L/D, SP PAD LOAD 1
037361,000097: # L/D DESIRED LIFT TO DRAG RATIO 1
037362,000098: # (VERTICAL PLANE)
037363,000099: # L/D1 TEMP STORAGE FOR L/D IN LATERAL 1
037364,000100: # L/DCMINR LAD COS(15DEG) 1 (NOM = 0.2895)
037365,000101: # PREDANGL PREDICTED RANGE (FINAL PHASE) 2700 NM = PREDANG
037366,000102: # Q2 FINAL PHASE RANGE 21600 NM
037367,000103: # Q7 MINIMUM DRAG FOR UPCONTROL 805FPSS
037368,000104: # RDOT ALTITUDE RATE 2 VSAT
037369,000105: # RDOTREF REFERENCE RDOT FOR UPCONTROL 2 VSAT
037370,000106: # RDOTREF( ) REFERENCE RDOT (FINAL PHASE TABLE) 2 VSAT = FX +3 /8
037371,000107: # RDTR REFERENCE RDOT FOR DOWNCONT 2 VSAT NOT SAVED
037372,000108: # ROLLC ROLL COMMAND 1 REVOLUTION
037373,000109: # RTOGO( ) RANGE TO GO (FINAL PHASE TABLE) 2700 NM = FX +2
037374,000110: # SL SINE OF LATITUDE 1 NOT SAVED
037375,000111: # T TIME B 28 CENTISEC = PIPTIME-TIME/RTO
037376,000112: # THETA DESIRED RANGE (RADIANS) 2 PI RADIANS = THETAH
037377,000113: # THETNM DESIRED RANGE (NM) 21600 NM NON EXISTENT
037378,000114: # V VELOCITY MAGNITUDE 2 VSAT
037379,000115: # V1 INITIAL VELOCITY FOR UPCONTROL 2 VSAT
037380,000116: # VL EXIT VELOCITY FOR UPCONTROL 2 VSAT
037381,000117: # VMAGI INERTIAL VELOCITY MAGNITUDE,|VI| 128 M/CENTISEC
037382,000118: # VREF REFERENCE VELOCITY FOR UPCONTROL 2 VSAT
037383,000119: # VREF( ) REFERENCE V (FINAL PHASE TABLE) 2 VSAT NOT STORED
037384,000120: # VS1 VSAT OR V1, WHICHEVER IS SMALLER 2 VSAT
037385,000121: # 2 2
037386,000122: # VBARS VL /VSAT 4
037387,000123: # 2 2
037388,000124: # VSQ NORMALISED VEL. SQUARED = V /VSAT 4 = VSQUARE
037389,000125:
037390,000126: # WT EARTH RATE TIMES TIME 1 REVOLUTION NOT SAVED
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037392,000128: # = WIE (DTEAROT)
037393,000129: # X INTERMEDIATE VARIABLE IN G-LIMITER 2 VSAT NOT SAVED
037394,000130: # Y LATERAL MISS LIMIT 4 RADIANS NOT SAVED
037395,000131:
037396,000132: # FIGURE 7.0-2A COMPUTER VARIABLES (CONTINUED)
037397,000133:
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037399,000135: # EXTRA COMPUTER ERASABLE LOCATIONS NOT SHOWN ON FLOW CHARTS
037400,000136: # -----------------------------------------------------------
037401,000137:
037402,000138: # VARIABLE DESCRIPTION MAXIMUM VALUE
037403,000139: # -------- ----------- ------- -----
037404,000140:
037405,000141: # GOTOADDR ADDRESS SELECTED BY SEQUENCER
037406,000142: # XPIPBUF BUFFER TO STORE X PIPA COUNTS
037407,000143: # YPIPBUF BUFFER TO STORE Y PIPA COUNTS
037408,000144: # ZPIPBUF BUFFER TO STORE Z PIPA COUNTS
037409,000145: # PIPCTR COUNTS PASSES THRU PIPA READ ROUTINE
037410,000146: # JJ INDEX IN FINAL PHASE TABLE LOOK-UP
037411,000147: # MM INDEX IN FINAL PHASE TABLE LOOK-UP
037412,000148: # GRAD INTERPOLATION FACTOR IN FINAL PHASE
037413,000149: # FX DRANGE/D L/D = F3 2700 NM
037414,000150: # FX + 1 AREF 805 FPSS
037415,000151: # FX + 2 RTOGO 2700 NM
037416,000152: # FX + 3 RDOTREF VSAT/4
037417,000153: # FX + 4 DRANGE/D RDOT = F2 21600/2VS NM/FPS
037418,000154: # FX + 5 DRANGE/D DRAG = F1 2700/805 NM/FPSS
037419,000155: # TEM1B TEMPORARY LOCATION
037420,000156: # TIME/RTO TIME OF INITIAL TARGET RTINIT B 28 CENTISEC
037421,000157: # DTEAROT EST TIME BETWEEN RTINIT AND RT B 28 CENTISEC
037422,000158: # -
037423,000159: # UNITV UNIT V VECTOR 2
037424,000160: # -
037425,000161: # UNITR UNIT R VECTOR 2
037426,000162: # -
037427,000163: # -VREL NEGATIVE VELOCITY REL TO ATMOSP 2 VSAT
037428,000164:
037429,000165: # COMPUTER SWITCHES INITIAL STATE CM/FLAGS = STATE +6
037430,000166: # -------- -------- ------------- -------------------
037431,000167:
037432,000168: # ENTRYDSP DO ENTRY DISPLAY, IF SET NON-BRANCH (1) 92D, BIT13
037433,000169: # GONEPAST INDICATES OVERSHOOT OF TARGET BRANCH (1) 95D, BIT10
037434,000170: # RELVELSW RELATIVE VELOCITY SWITCH NON-BRANCH (0) 96D, BIT 9
037435,000171: # EGSW FINAL PHASE SWITCH NON-BRANCH (0) 97D, BIT 8
037436,000172: # NOSWITCH INHIBIT LATERAL SWITCH NON-BRANCH (0) 98D, BIT 7
037437,000173: # HIND INDICATES ITERATION IN HUNTEST NON-BRANCH (0) 99D, BIT 6
037438,000174: # INRLSW INDICATES INIT ROLL ATTITUDE SET NON-BRANCH (0) 100D, BIT 5
037439,000175: # LATSW INHIBIT DOWNLIFT SWITCH IF NOT SET BRANCH (1) 101D, BIT 4
037440,000176: # .05GSW INDICATES DRAG EXCEEDS .05 GS NON-BRANCH (0) 102D, BIT 3
037441,000177:
037442,000178: # GONEBY INDICATES GONE PAST TARGET (SET) SELF-INITIALIZING 112D, BIT 8 IN STATE +7
037443,000179:
037444,000180: # FIGURE 7.0-2B COMPUTER VARIABLES (CONTINUED)
037445,000181:
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037447,000183: # BODY ATTITUDE QUANTITIES (CM/POSE)
037448,000184: # -----------------------------------
037449,000185:
037450,000186: # VARIABLE DECRIPTION MAXIMUM VALUE
037451,000187: # -------- ---------- ------- -----
037452,000188: # -
037453,000189: # -VREL NEGATIVE VELOCITY REL TO ATMOS. 2 VSAT
037454,000190: # - -
037455,000191: # OLDUYA USED FOR UYA BELOW 1000 FPS 2
037456,000192:
037457,000193: # -
037458,000194: # UXA/2 UNIT VECTOR TRIAD 2
037459,000195: # -
037460,000196: # UYA/2 BASED ON 2
037461,000197: # -
037462,000198: # UZA/2 THE TRAJECTORY. 2
037463,000199:
037464,000200: # -
037465,000201: # UBX/2 UNIT VECTOR 2
037466,000202: # -
037467,000203: # UBY/2 BODY TRIAD 2
037468,000204: # -
037469,000205: # UBZ/2 FOR CM. 2
037470,000206:
037471,000207: # FIGURE 7.0-2C COMPUTER VARIABLES (CONTINUED)
037472,000208:
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037474,000210: # DISPLAY QUANTITIES (FOR USAGE,SEE SECTION 4: P 61 THROUGH P 67)
037475,000211: # ------------------
037476,000212:
037477,000213: # THIS TABLE PROVIDES THE READER WITH DISPLAY QUANTITY INFORMATION. THE VARIABLE NAMES REFLECT
037478,000214: # SECTION 5 USAGE. EXCEPTING IMBEDDED BLANKS, THE SECTION 4 NAMES ARE PARENTHESIZED,IF DIFFERENT.
037479,000215: # SIGN CONVENTIONS ARE FOUND IN SECTION 4. IF THE DISPLAY VARIABLE NAME DIFFERS FROM SECTION 5 USAGE,
037480,000216: # SAY BECAUSE OF SCALE FACTOR, THE ALTERNATE SECTION 5 NAME IS ENCLOSED IN ANGULAR BRACKETS: < >.
037481,000217: # DISPLAY QUANTITY INFORMATION APPEARING ELSEWHERE IN SECTION 5 OTHER THAN IN 5 7 MAY BE FOUND THUS:
037482,000218: # N 60 & N 63 (ALL) FIGURE 6.10-4 IN 5.6.10.3
037483,000219: # N 22 (ALL) FIGURE 6.10-11 IN 5.6.10.6
037484,000220: # N67 (LAT, LONG) FIGURE 5.3-1 IN 5.5.3
037485,000221:
037486,000222: # VARIABLE DESCRIPTION MAXIMUM VALUE DISPLAY NOUNS
037487,000223: # -------- ----------- ------- ----- ------- -----
037488,000224:
037489,000225: # GMAX PREDICTED MAXIMUM ENTRY ACCEL 163.84 GS N 60
037490,000226: # VPRED PREDICTED VELOCITY AT ALTITUDE 128 M/CENTISEC N 60
037491,000227: # 400K FT ABOVE FISCHER RADIUS.
037492,000228: # GAMMAEI PREDICTED GAMMA AT ALTITUDE 1 REVOLUTION N 60
037493,000229: # 400K FT ABOVE FISCHER RADIUS.
037494,000230: # RTGO RANGE ANGLE TO SPLASH (RTOGO) 1 REVOLUTION N 63
037495,000231: # FROM EMSALT FT ABOVE FISCHER
037496,000232: # RADIUS. (IN NM)
037497,000233: # VIO PREDICTED VELOCITY AT ALTITUDE 128 M/CENTISEC N 63
037498,000234: # EMSALT FT ABOVE FISCHER RADIUS.
037499,000235: # TTE TIME OF FREE FALL (TFE) TO B 28 CENTISEC N 63
037500,000236: # ALTITUDE EMSALT FT ABOVE FISCHER
037501,000237: # RADIUS.
037502,000238: # OGA OUTER GIMBAL ANGLE (OG ROLL) 1 REVOLUTION N 22
037503,000239: # IGA INNER GIMBAL ANGLE (IG PITCH) 1 REVOLUTION N 22
037504,000240: # MGA MIDDLE GIMBAL ANGLE (MG YAW) 1 REVOLUTION N 22
037505,000241: # ALL ABOVE ANGLES FOR HYPERSONIC TRIM
037506,000242: # D DRAG ACCELERATION (G) 805 FPSS N 64, N 74
037507,000243: # VMAGI INERTIAL VELOCITY MAGNITUDE (VI) 128 M/CENTISEC N 64, N 68, N 74
037508,000244: # ROLLC ROLL COMMAND (BETA) 1 REVOLUTION N 66, N 68, N 69, N 74
037509,000245: # XRNGERR CROSS-RANGE ERROR <LATANG IN NM> 1 REVOLUTION N 66
037510,000246: # DNRNGERR DOWN RANGE ERROR ** 1 REVOLUTION N 66
037511,000247: # <PREDANG - THETAH IN NM>
037512,000248: # ** <DNRNGERR DISPLAYS 9999.9 IF GONEPAST =1 IN P 67>
037513,000249: # HDOT ALTITUDE RATE <RDOT> 128 M/CENTISEC N 68
037514,000250: # Q7 EXIT DRAG LEVEL (DL) 805 FPSS N 69
037515,000251: # VL EXIT VELOCITY FOR UP-CONTROL 2 VSAT N 69
037516,000252: # RTOGO DESIRED RANGE ANGLE <THETAH> 1 REVOLUTION N 67, N 64
037517,000253: # <-THETAH IF GONEBY =0, THETAH IF GONEBY =1>
037518,000254: # LAT GEODETIC LATITUDE OF VEHICLE 1 REVOLUTION N 67
037519,000255: # LONG LONGITUDE OF VEHICLE 1 REVOLUTION N 67
037520,000256:
037521,000257: # THE FOLLOWING IS A DATA INPUT NOUN (REFER TO SECTION 4,P 61 & P 62)
037522,000258: # HEADSUP INDICATOR FOR INITIAL ROLL 1 REVOLUTION N 61
037523,000259: # LAT(SPL) GEODETIC LATITUDE OF TARGET 1 REVOLUTION N 61
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037525,000261: # (IMPACT LAT)
037526,000262: # LNG(SPL) LONGITUDE OF TARGET (IMPACT LONG) 1 REVOLUTION N 61
037527,000263:
037528,000264: # FIGURE 7.0-2D COMPUTER VARIABLES (CONTINUED)
037529,000265:
037530,000266:
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037532,000268: # CONSTANTS AND GAINS VALUE
037533,000269: # ------------------- -----
037534,000270:
037535,000271: # C1 FACTOR IN ALP COMPUTATION 1.25
037536,000272: # C16 CONSTD GAIN ON DRAG 0.01
037537,000273: # C17 CONSTD GAIN ON RDOT 0.002
037538,000274: # C18 BIAS VEL. FOR FINAL PHASE START 500 FPS
037539,000275: # C20 MAX DRAG FOR DOWN-LIFT 210 FPSS
037540,000276: # C21 DRAG FOR NO LATERAL SWITCH 140 FPSS
037541,000277: # CHOOK FACTOR IN AHOOK COMPUTATION 0.25
037542,000278: # CH1 FACTOR IN GAMMAL COMPUTATION 1.0
037543,000279: # COS15 COS( 15 DEG) 0.965
037544,000280: # DLEWD0 INITIAL VARIATION IN LEWD -0.05
037545,000281: # DT COMPUTATION CYCLE TIME INTERVAL 2 SEC.
037546,000282: # GMAX MAXIMUM ACCELERATION 257.6 FPSS (8 G-S)
037547,000283: # KA1 FACTOR IN KA CALC 1.3 GS
037548,000284: # KA2 FACTOR IN KA CALC 0.2 GS
037549,000285: # KA3 FACTOR IN D0 CALC 90 FPSS
037550,000286: # KA4 FACTOR IN D0 CALC 40 FPSS
037551,000287: # KB1 OPTIMIZED UPCONTROL GAIN 2.5
037552,000288: # KB2 OPTIMIZED UPCONTROL GAIN 0.0025
037553,000289: # KDMIN INCREMENT ON Q7F TO DETECT END OF KEPLER PHASE 0.5 FPSS
037554,000290: # KTETA TIME OF FLIGHT CONSTANT 1000
037555,000291: # KLAT1 FACTOR IN KLAT CALC 1/24
037556,000292: # K44 GAIN USED IN INITIAL ROLL SECTION 19749550 FPS
037557,000293: # LATBIAS LATERAL SWITCH BIAS TERM 0.41252961 NM
037558,000294: # LEWD1 NOMINAL UPCONTROL L/D 0.15
037559,000295: # POINT1 FACTOR TO REDUCE UPCONTROL GAIN 0.1
037560,000296: # Q3 FINAL PHASE DRANGE/D V 0.07 NM/FPS
037561,000297: # Q5 FINAL PHASE DRANGE/ D GAMMA 7050 NM/RAD
037562,000298: # Q6 FINAL PHASE INITIAL FLIGHT PATH ANGLE 0.0349 RAD
037563,000299: # Q7F MIN DRAG FOR UPCONTROL 6 FPSS
037564,000300: # Q7MIN MIN VALUE FOR Q7 IN FACTOR CALCULATION 805 FPSS (DISABLE FACTOR)
037565,000301: # Q19 FACTOR IN GAMMAL1 CALCULATION 0.5
037566,000302: # Q21 FACTOR IN Q2 CALCULATION. 3500 NM
037567,000303: # Q22 FACTOR IN Q2 CALCULATION. -1992 NM
037568,000304: # VFINAL1 VELOCITY TO START FINAL PHASE ON INITIAL ENTRY 27000 FPS
037569,000305: # VFINAL FACTOR IN INITIAL UP-DOWN CALC 26600 FPS
037570,000306: # VLMIN MINIMUM VL 18000 FPS
037571,000307: # VMIN VELOCITY TO SWITCH TO RELATIVE VEL VSAT/2
037572,000308: # VRCONTRL RDOT TO START INTO HUNTEST 700 FPS
037573,000309: # VRCONT = COMPUTER NAME
037574,000310: # 25NM TOLERANCE TO STOP RANGE ITERATION 25 NM
037575,000311: # VQUIT VELOCITY TO STOP STEERING 1000 FPS
037576,000312:
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037578,000314: # CONVERSION FACTORS AND SCALING CONSTANTS
037579,000315: # ---------- ------- --- ------- ---------
037580,000316:
037581,000317: # ATK ANGLE IN RAD TO NM 3437.7468 NM/RAD
037582,000318: # GS NOMINAL G VALUE FOR SCALING 32.2 FPSS
037583,000319: # HS ATMOSPHERE SCALE HEIGHT 28500 FT
037584,000320: # J GRAVITY HARMONIC COEFFICIENT 0.00162346
037585,000321: # KWE EQUATORIAL EARTH RATE 1546.70168 FPS
037586,000322: # MUE EARTH GRAVITATIONAL CONSTANT 3.986032233 E 14 CUBIC M/ SEC SEC
037587,000323: # RE EARTH RADIUS 21202900 FT
037588,000324: # REQ EARTH EQUATORIAL RADIUS 20925738.2 FT
037589,000325: # VSAT SATELLITE VELOCITY AT RE 25766.1973 FPS
037590,000326: # WIE EARTH RATE 0.0000729211505 RAD/SEC
037591,000327:
037592,000328: # FIGURE 7.0-3 CONSTANTS, GAINS AND CONVERSION FACTORS
End of include-file ENTRY_LEXICON.agc. Parent file is MAIN.agc