Source Code
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These source-code files are part of a reconstructed copy of Comanche 72/3 (AKA Manche72 revision 3),
the final, flown mission release of the Apollo Guidance Computer (AGC) Command Module (CM) software
for Apollo 13.
The starting point was the source code of Comanche 72 (itself previously reconstructed). Comanche 72
source code was then modified by incorporating changes known from contemporary documentation to have
been made between revisions 72 and 72/3. The resulting code assembles to have identical
memory-bank checksums as those specified in NASA drawing 2021153G; this gives reasonably
high confidence that the changes that have been made are correct. In places where
ambiguity exists, this ambiguity is discussed in "## Reconstruction:" comments.
Since no contemporary listings of Comanche 72/3 are available as source material,
all comments and labels are approximate.
They have been taken from other AGC programs where possible, or, in some places, written
from scratch to match what we believe would have been in the original listing.
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011981,000002: ## Copyright: Public domain.
011982,000003: ## Filename: CSM_GEOMETRY.agc
011983,000004: ## Purpose: A section of Manche72 revision 3.
011984,000005: ## It is part of the reconstructed source code for the final, flown
011985,000006: ## release of the software for the Command Module's (CM) Apollo
011986,000007: ## Guidance Computer (AGC) for Apollo 13. No original listings
011987,000008: ## of this program are available; instead, this file was recreated
011988,000009: ## from a reconstructed copy of Comanche 072. It has been adapted
011989,000010: ## such that the resulting bugger words exactly match those
011990,000011: ## specified for Manche72 revision 3 in NASA drawing 2021153G,
011991,000012: ## which gives relatively high confidence that the reconstruction
011992,000013: ## is correct.
011993,000014: ## Assembler: yaYUL
011994,000015: ## Contact: Ron Burkey <info@sandroid.org>.
011995,000016: ## Website: www.ibiblio.org/apollo/index.html
011996,000017: ## Mod history: 2024-05-19 MAS Created from Comanche 072.
011997,000018:
011998,000019: 22,2000 BANK 22
011999,000020: 23,2000 SETLOC COMGEOM1
012000,000021: 23,2000 BANK
012001,000022:
012002,000023: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012003,000024: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012004,000025:
012005,000026: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012006,000027: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012007,000028: # JOB VAC AREA.
012008,000029:
012009,000030: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012010,000031: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012011,000032:
012012,000033: 23,2000 COUNT 23/GEOM
012013,000034:
012014,000035: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012015,000036: 23,2001 00006 5,1 # TRUNNION = TA
012016,000037: 23,2002 45513 CDULOGIC
012017,000038: 23,2003 41434 RTB PUSH
012018,000039: 23,2004 46027 SXTLOGIC
012019,000040: 23,2005 72556 SIN SL1
012020,000041: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012021,000042: 23,2007 00004 3,1 # SHAFT = SA
012022,000043: 23,2010 41434 RTB PUSH # PD4 = SA
012023,000044: 23,2011 45513 CDULOGIC
012024,000045:
012025,000046: 23,2012 41346 COS DMP
012026,000047: 23,2013 00003 2
012027,000048: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012028,000049:
012029,000050: 23,2015 41356 SIN DMP
012030,000051: 23,2016 77626 STADR
012031,000052: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012032,000053:
012033,000054: 23,2020 77746 COS
012034,000055: 23,2021 24045 STOVL STARM +4
012035,000056: 23,2022 00041 STARM # STARM = 32D
012036,000057: 23,2023 76521 MXV VSL1
012037,000058: 23,2024 06302 NB1NB2
012038,000059: 23,2025 00041 STORE 32D
012039,000060: 23,2026 77616 RVQ
012040,000061:
012041,000062: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012042,000063: 23,2030 26154 ADS MPAC
012043,000064: 23,2031 35017 CAF QUARTER
012044,000065: 23,2032 07256 TC SHORTMP
012045,000066: 23,2033 06030 TC DANZIG
012046,000067:
012047,000068: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012048,000069: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012049,000070: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012050,000071: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012051,000072:
012052,000073: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012053,000074: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012054,000075: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012055,000076:
012056,000077: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012057,000078: # EQUAL TO ZERO).
012058,000079:
012059,000080: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012060,000081: 23,2035 00034 28D
012061,000082: 23,2036 02766 STAR
012062,000083: 23,2037 77624 CALL
012063,000084: 23,2040 47646 *SMNB*
012064,000085: 23,2041 76521 MXV VSL1
012065,000086: 23,2042 06260 NB2NB1
012066,000087: 23,2043 26766 STOVL STAR
012067,000088: 23,2044 15332 HIUNITX
012068,000089: 23,2045 26555 STOVL XNB1
012069,000090: 23,2046 15330 HIUNITY
012070,000091: 23,2047 26563 STOVL YNB1
012071,000092: 23,2050 15326 HIUNITZ
012072,000093: 23,2051 36571 STCALL ZNB1
012073,000094: 23,2052 46076 SXTANG1
012074,000095:
012075,000096: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012076,000097: # SIGHT LIES ALONG THE STAR VECTOR.
012077,000098:
012078,000099: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012079,000100: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012080,000101: # ZNB.
012081,000102:
012082,000103: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012083,000104: # EQUAL TO ZERO).
012084,000105:
012085,000106: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012086,000107: 23,2054 00034 28D
012087,000108: 23,2055 45662 TRANSP1 # EREF WRT NB2
012088,000109: 23,2056 64375 VLOAD MXV
012089,000110: 23,2057 02714 XNB
012090,000111: 23,2060 06260 NB2NB1
012091,000112: 23,2061 77772 VSL1
012092,000113: 23,2062 26555 STOVL XNB1
012093,000114: 23,2063 02722 YNB
012094,000115: 23,2064 76521 MXV VSL1
012095,000116: 23,2065 06260 NB2NB1
012096,000117: 23,2066 26563 STOVL YNB1
012097,000118: 23,2067 02730 ZNB
012098,000119: 23,2070 76521 MXV VSL1
012099,000120: 23,2071 06260 NB2NB1
012100,000121: 23,2072 02571 STORE ZNB1
012101,000122:
012102,000123: 23,2073 47034 RTB RTB
012103,000124: 23,2074 45662 TRANSP1
012104,000125: 23,2075 45676 TRANSP2
012105,000126:
012106,000127: 23,2076 47375 SXTANG1 VLOAD VXV
012107,000128: 23,2077 02571 ZNB1
012108,000129: 23,2100 02766 STAR
012109,000130: 23,2101 77600 BOV
012110,000131: 23,2102 46103 +1
012111,000132: 23,2103 40056 UNIT BOV
012112,000133: 23,2104 46145 ZNB=S1
012113,000134: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012114,000135:
012115,000136: 23,2106 57441 DOT DCOMP
012116,000137: 23,2107 02555 XNB1
012117,000138: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012118,000139: 23,2111 00027 PDA
012119,000140:
012120,000141: 23,2112 77641 DOT
012121,000142: 23,2113 02563 YNB1
012122,000143: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012123,000144: 23,2115 47260 ARCTRIG
012124,000145: 23,2116 77634 RTB
012125,000146: 23,2117 45546 1STO2S
012126,000147: 23,2120 26774 STOVL SAC
012127,000148: 23,2121 02766 STAR
012128,000149: 23,2122 77600 BOV
012129,000150: 23,2123 46124 +1
012130,000151: 23,2124 72441 DOT SL1
012131,000152: 23,2125 02571 ZNB1
012132,000153: 23,2126 77726 ACOS
012133,000154: 23,2127 62440 BMN SL2
012134,000155: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012135,000156: 23,2131 45200 BOV DSU
012136,000157: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012137,000158: 23,2133 06331 20DEG-
012138,000159: 23,2134 77634 RTB
012139,000160: 23,2135 45546 1STO2S
012140,000161: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012141,000162: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012142,000163: 23,2140 01630 CULTFLAG
012143,000164: 23,2141 00034 28D
012144,000165: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012145,000166: 23,2143 01430 CULTFLAG
012146,000167: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012147,000168: 23,2145 77745 ZNB=S1 DLOAD
012148,000169: 23,2146 06325 270DEG
012149,000170: 23,2147 16774 STODL SAC
012150,000171: 23,2150 06327 20DEGS-
012151,000172: 23,2151 02776 STORE PAC
012152,000173: 23,2152 77614 CLRGO
012153,000174: 23,2153 01630 CULTFLAG
012154,000175: 23,2154 00034 28D
012155,000176:
012156,000177: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012157,000178: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012158,000179: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012159,000180: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012160,000181: # OTHER VEHICLES COMPUTER.
012161,000182:
012162,000183: # INPUT
012163,000184: # STATE VECTOR IN TEMPORARY STORAGE AREA
012164,000185: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012165,000186: # SET X2 TO +2
012166,000187: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012167,000188: # SET X2 TO 0
012168,000189:
012169,000190: # OUTPUT
012170,000191: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012171,000192: # OR
012172,000193: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012173,000194:
012174,000195: 23,2155 BANK 23
012175,000196: 10,2000 SETLOC COMGEOM2
012176,000197: 10,2000 BANK
012177,000198: 10,2237 COUNT 10/GEOM
012178,000199: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012179,000200: 10,2240 04756 AVEMIDSW
012180,000201: 10,2241 20242 +1
012181,000202: 10,2242 53775 VLOAD VSL*
012182,000203: 10,2243 01521 TDELTAV
012183,000204: 10,2244 57605 0 -7,2
012184,000205: 10,2245 53655 VAD VSL*
012185,000206: 10,2246 01535 RCV
012186,000207: 10,2247 57576 0,2
012187,000208: 10,2250 25171 STOVL RN
012188,000209: 10,2251 01527 TNUV
012189,000210: 10,2252 53257 VSL* VAD
012190,000211: 10,2253 57602 0 -4,2
012191,000212: 10,2254 01543 VCV
012192,000213: 10,2255 77657 VSL*
012193,000214: 10,2256 57576 0,2
012194,000215: 10,2257 15177 STODL VN
012195,000216: 10,2260 01517 TET
012196,000217: 10,2261 01205 STORE PIPTIME
012197,000218: 10,2262 77616 RVQ
012198,000219:
012199,000220: 10,2263 53775 SVDWN2 VLOAD VSL*
012200,000221: 10,2264 01521 TDELTAV
012201,000222: 10,2265 57605 0 -7,2
012202,000223: 10,2266 53655 VAD VSL*
012203,000224: 10,2267 01535 RCV
012204,000225: 10,2270 57576 0,2
012205,000226: 10,2271 25722 STOVL R-OTHER
012206,000227: 10,2272 01527 TNUV
012207,000228: 10,2273 53257 VSL* VAD
012208,000229: 10,2274 57602 0 -4,2
012209,000230: 10,2275 01543 VCV
012210,000231: 10,2276 77657 VSL*
012211,000232: 10,2277 57576 0,2
012212,000233: 10,2300 01730 STORE V-OTHER
012213,000234: 10,2301 77616 RVQ
012214,000235:
012215,000236: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012216,000237:
012217,000238: # ENTRY: CALL
012218,000239: # LOG
012219,000240:
012220,000241: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012221,000242:
012222,000243: # EBANK IS ARBITRARY..
012223,000244:
012224,000245: 14,2000 BANK 14
012225,000246: 23,2000 SETLOC POWFLIT2
012226,000247: 23,2000 BANK
012227,000248: 23,2155 COUNT 23/GEOM
012228,000249:
012229,000250: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012230,000251: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012231,000252: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012232,000253: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012233,000254: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012234,000255: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012235,000256: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012236,000257: 23,2165 01001 14636 2DEC .031335467
012237,000258: 23,2167 00325 07310 2DEC .0130145859
012238,000259: 23,2171 00541 16735 2DEC .0215738898
012239,000260:
012240,000261: 23,2173 35035 CAF ZERO
012241,000262: 23,2174 54156 TS MPAC +2
012242,000263: 23,2175 00006 EXTEND
012243,000264: 23,2176 32214 DCA CLOG2/32
012244,000265: 23,2177 52155 DXCH MPAC
012245,000266: 23,2200 52160 DXCH MPAC +3
012246,000267: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012247,000268: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012248,000269:
012249,000270: 23,2203 52156 DXCH MPAC +1
012250,000271: 23,2204 52155 DXCH MPAC
012251,000272: 23,2205 52160 DXCH MPAC +3
012252,000273: 23,2206 20155 DAS MPAC
012253,000274: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012254,000275:
012255,000276: 23,2210 77616 RVQ
012256,000277:
012257,000278: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012258,000279:
012259,000280: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012260,000281:
012261,000282: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012262,000283: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012263,000284: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012264,000285:
012265,000286: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012266,000287: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012267,000288: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012268,000289: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012269,000290: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012270,000291: # THE EQUATIONS ARE
012271,000292: # - - - -
012272,000293: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012273,000294:
012274,000295: # WHERE WT = WIE DTEAROT
012275,000296:
012276,000297: # RTINIT = INITIAL TARGET VECTOR
012277,000298: # - - -
012278,000299: # RTEAST = UNITW * RTINIT
012279,000300: # - - -
012280,000301: # RTNORM = RTEAST * UNITW
012281,000302:
012282,000303: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012283,000304: #
012284,000305: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012285,000306: # STCALL DTEAROT STCALL DTEAROT
012286,000307: # EARROT1 EARROT2
012287,000308: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012288,000309: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012289,000310:
012290,000311: # SUBROUTINES USED: NONE
012291,000312:
012292,000313: # NORMAL EXIT MODES: RVQ
012293,000314:
012294,000315: # ALARMS: NONE
012295,000316:
012296,000317: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012297,000318: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012298,000319: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012299,000320: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012300,000321:
012301,000322: # ERASABLE INITIALIZATION REQUIRED:
012302,000323: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012303,000324: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012304,000325: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012305,000326:
012306,000327: # DEBRIS: QPRET, PDL+0 ... PDL+5
012307,000328: 23,2215 E7,1451 EBANK= RTINIT
012308,000329:
012309,000330: 23,2215 47375 EARROT1 VLOAD VXV
012310,000331: 23,2216 01714 UNITW # FULL UNIT VECTOR
012311,000332: 23,2217 03452 RTINIT # .5 UNIT
012312,000333: 23,2220 03460 STORE RTEAST # .5 UNIT
012313,000334:
012314,000335: 23,2221 77635 VXV
012315,000336: 23,2222 01714 UNITW # FULL UNIT
012316,000337: 23,2223 17466 STODL RTNORM # .5 UNIT
012317,000338: 23,2224 03606 DTEAROT # (-28) CS
012318,000339:
012319,000340: 23,2225 56204 EARROT2 BOVB DDV
012320,000341: 23,2226 57353 TCDANZIG # RESET OVFIND, IF ON
012321,000342: 23,2227 06256 1/WIE
012322,000343: 23,2230 41400 BOV PUSH
012323,000344: 23,2231 46245 OVERADAY
012324,000345: 23,2232 45346 COS DSU
012325,000346: 23,2233 15332 HIDPHALF
012326,000347: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012327,000348: 23,2235 03466 RTNORM # .5 UNIT
012328,000349: 23,2236 74356 SIN VXSC
012329,000350: 23,2237 03460 RTEAST # .5 UNIT
012330,000351: 23,2240 76455 VAD VSL1
012331,000352: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012332,000353: 23,2242 03452 RTINIT # .5 UNIT
012333,000354: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012334,000355:
012335,000356: 23,2244 77616 RVQ
012336,000357:
012337,000358: 23,2245 75345 OVERADAY DLOAD SIGN
012338,000359: 23,2246 06256 1/WIE
012339,000360: 23,2247 03606 DTEAROT
012340,000361: 23,2250 77621 BDSU
012341,000362: 23,2251 03606 DTEAROT
012342,000363: 23,2252 03606 STORE DTEAROT
012343,000364:
012344,000365: 23,2253 77650 GOTO
012345,000366: 23,2254 46225 EARROT2
012346,000367:
012347,000368: # WIE 2DEC .1901487997
012348,000369: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012349,000370: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012350,000371: 23,2261 00000 00000 2DEC 0 B-28
012351,000372: 23,2263 67313 65307 2DEC -.5376381241 B-1
012352,000373: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012353,000374: 23,2267 20000 00000 HALFNFLT 2DEC .5
012354,000375: 23,2271 00000 00000 2DEC 0 B-28
012355,000376: 23,2273 10464 12470 2DEC +.5376381241 B-1
012356,000377: 23,2275 00000 00000 2DEC 0 B-28
012357,000378: 23,2277 15373 11346 2DEC +.8431756920 B-1
012358,000379: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012359,000380: 23,2303 00000 00000 2DEC 0 B-28
012360,000381: 23,2305 10464 12470 2DEC +.5376381241 B-1
012361,000382: 23,2307 00000 00000 2DEC 0 B-28
012362,000383: 23,2311 20000 00000 2DEC .5
012363,000384: 23,2313 00000 00000 2DEC 0 B-28
012364,000385: 23,2315 67313 65307 2DEC -.5376381241 B-1
012365,000386: 23,2317 00000 00000 2DEC 0 B-28
012366,000387: 23,2321 15373 11346 2DEC +.8431756920 B-1
012367,000388: 23,2323 07020 10DEGS- DEC 3600 B-14
012368,000389: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012369,000390: 23,2325 00000 OCT 00000
012370,000391: 23,2326 61740 20DEGS- DEC -07199 B-14
012371,000392: 23,2327 77777 DEC -00000 B-14
012372,000393: 23,2330 07020 20DEG- DEC 03600 B-14
012373,000394: 23,2331 00000 DEC 00000 B-14
012374,000395:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc