user manual

TABLE 3.2-10 (CONTINUED)
MISSION J-2
Command Module Water and GOX
Waste Water 6
Potable Water ?
CM/COX
Pressure
(PSIA)
900±50
Loading Requirement
Weight _ib)
3.7
Amendment 114
9/15/71
Earth Launch
Weight (lb)
35.0
30.0
6.7 (Entry)
Actual
8Service Module Hydrogen and Oxygen
Hydrogen
Tank i
Tank 2
Tank 3
Oxygen
Tank i
Tank 2
Tank 3
Loading Req. Per Tank
(pounds)
29.3
29.3
29.3
330.1
330 .i
330.1
Earth Launch Weight
Per Tank (ib)
27.6
27.6
27.6
316.6
316.6
316.6
Actual
Per Tank (Ib I
NOTES :
11ndicated propellant load is based on nominal pressure and temperature
prior to actual loading. This number will be updated after loading is
accomplished.
2See Section 4.1 for explanation of trapped SPS propellant.
3See Table 3.2-13 for loading uncertainties.
4See Section 4.2 for SM/RCS loads and uncertainties to be used in Mission
Planning. Actual SM/RCS loads and uncertainties will be published in
Table 3.2-15.
5See Section 4.2 for CM/RCS loads and uncertainties to be used in Mission
Planning. Actual CM/RCS loads and uncertainties will be published in
Table 3.2-14.
6Launch Rule Redlines determine lift-off values.
7Launch Rule Redlines determine lift-off values.
8Launch Mission Rules will determine minimum llft-off quantities for H 2
and 02 .
9CSM helium and nitrogen should be loaded in accordance with loading win-
dows contained in CSM/LM Spacecraft Operational Data Book, Volume I, Part
2, SNA-8-D-027(1) P2.
3.2-97 SNA-8-D-O27(III)REV 3