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SCORE-Bench

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1959 1961 1963 1965 1967 1969 1971 1973 1975 1977 1979 1981 1983 1985 1987 1989 1991 1993 1995 1997 1999 2001 2003 2005 2007 2009 2011 2013 2015 2017 2019 2021 2023
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Amount Projected
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https://www.planetary.org/get-involved/be-a-space-advocate/nasa-budget.html
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(Integrated by eye)
Total = $25 billion * (2013-1959) + ½ * (1971-1962) * $35 billion
Takeaway: Sending humans to Mars is an expensive and hard problem. NASA cannot pick up the whole tab without support.
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Amendment 110 7/19/71
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XA COORDINATES
TABLE 3.1-2 (CONTINUED)
CSM 112/LM10 EXPECTED SEQUENTIAL MASS PROPERTIES
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DESCRIPTION S WEIGHT POUNDS C.G. INCHES INERTIAS SLUG-FT2 PRODUCTS SLUG-FT2 DISPERSIONS LB/IN
X Y Z IXX IYY IZZ PXY PXZ PYZ D DX DY DZ
CSM AT EARTH LAUNCH 66924.8 933.9 5.0 4.7 36397 80079 81729 -2101 272 2247 193.6 .4 .2 .2
LM AT EARTH LAUNCH 36237.7 583.6 .4 -.9 25859 27364 26117 87 515 192 42.3 .4 .2 .2
SLA (EXCLUDING RING) 3964.2 638.9 .6 -.2 9996 12495 12470 -47 116 28 25.0 1.0 .5 .5
LES 9108.0 1298.8 .2 .8 832 28026 28082 42 799 1 25.0 1.0 .5 .5
CSM+LM+SLA+LES AT LAUNCH 116234.7 843.2 3.1 2.5 73391 1237 47 1238236 3773 10529 2617 201.3 .3 .2 .2
CSM+LM+SLA AT E.O.1. 107126.7 804.5 3.3 2.6 72536 767108 767430 6506 11356 2605 199.8 .4 .2 .2
CSM+LM+SLA PRE TRANS/DOCK 107123.1 804.5 3.3 2.6 72537 767132 767460 6491 11347 2608 199. .4 .2 .2
CSM AT TRANS/DOCK 66850.6 933.9 5.0 4.7 36324 80036 81701 -2111 273 2268 193.6 .4 .2 .2
LM AT TRANS/DOCK 36235.0 1238.2 -.6 .8 25854 26153 27114 -491 186 -445 42.3 .4 .3 .1
CSM/LM DOCKED 103085.6 1040.9 3.0 3.3 62416 575831 598541 - 11282 -5531 1934 198.2 .4 .2 .2
CM EQUIP.RELOC.1 - 531.6 1042.6 -9.0 -11.8 36 7 33 0 1 0 .0 .0 .0 .0
CM EQUIP.RELOC.1 + 531.6 1034.2 -8.4 -13.6 30 33 43 -8 7 -1 .0 .0 .0 .0
SIM DOOR - 160.0 912.1 43.2 -59.5 20 65 85 0 0 0 .0 .0 .0 .0
CM GASEOUS O2 + 5.5 1168.7 13.0 -7.5 0 0 0 0 0 0 .0 .0 .0 .0
CSM/LM PRE L.O.1. 102692.0 1041.3 3.0 3.5 62028 574327 577101 - 11117 -5805 2075 198.2 .4 .2 .2
CSM/LM POST L.O.1. 76391.8 1083.6 1.9 2.0 48396 443223 449320 -8697 -1220 -1030 198.2 .7 .2 .2
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3.1-4
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SNA-B-D-027(III) REV 3
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TABLE 4.3-5
SERVICE MODULE RCS LOADING PARAMETERS AND CALCULATIONS - QUAD C
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Fuel
Secondary Fuel
A. Loading Temperature (°F) ___
B. Tank Volume (in³) @ 0.0 PSIG ___
B1. Liquid Line Volume (in³) ___
C. Tank Stretch Factor (in³/PSI) 0.034
D. Initial Weight of Bleed Unit Prior to Loading (lb) ___
E. Final Weight of Bleed Unit After Loading (lb) ___