Page:LunarLandingMIssionSymposium1966 1978075303.pdf/93

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{{left|NASA-S-66-6585 JUN

APOLLO SPACECRAFT WEIGHT DATA
  CURRENT
(LBS)
PREDICTED
(LBS)
MAXIMUM
(LBS)
COMMAND MODULE
(INCL CREW)
11,755 12,050 12,250
SERVICE MODULE 10,300 11,250 11,300
SM BAY PAYLOAD 0 0 1000
SPS PROPELLANT 37,075 38,800 38,964
LUNAR MODULE
(NOT INCL CREW)
30,755 32,000 32,486
SC/LM ADAPTER 3755 3900 4000
TOTAL 93,640 98,000 100,000

Fig. 65

NASA-S-66-6586 JUN
LUNAR MODULE WEIGHT BREAKDOWN
  PREDICTED
(LBS)
MAXIMUM
(LBS)
CURRENT
(LBS)
ASCENT STAGE 4450 4620 4645
RCS PROPELLANT 507 540 540
APS PROPELLANT 4538 4810 4921
DESCENT STAGE 4685 4795 4795
DPS PROPELLANT 16,575 17,235 17,585
TOTAL 30,755 32,000 32,486

Fig. 66

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