user manual

TABLE 3.5-10 (Continued)
Command Module Water and GOX
Amendment 86
9/10/70
Waste Water6
Potable Water 7
CM/GOX
Pressure
(PSIA)
900±50
Loading Requirement
Weight (ib)
3.7
Earth Launch
Weight (ib)
18.0
36.0
6.7 (Entry)
8Service Module Hydrogen and Oxygen
Hydrogen
Tank 1
Tank 2
Tank 3
Oxygen
Tank 1
Tank 2
Tank 3
Loading Req. Per Tank
(pounds)
Earth Launch Weight
29.3
29.3
29.3
330.1
330.1
330.1
Per Tank (ib)
27.6
27.6
27.6
316.6
316.6
316.6
Actual
NOTES:
llndicated 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 3.5-13 for loading uncertainties.
4See Section 4.2 for SM/RCS loads and uncertainties to be used in Mis-
sion Planning. Actual SM/RCS loads and uncertainties will be published
in Table 3.5-15.
5See Section 4.2 for CM/RCS loads and uncertainties to be used in Mis-
sion Planning. Actual CM/RCS loads and uncertainties will be published
in Table 3.5-14.
6Launch Rule Redlines determine lift-off values.
7Launch Rule Redlines determine lift-off values.
8Launch Mission Rules will determine minimum lift-off quantities for
H 2 and 02 .
9CSM helium and nitrogen should be loaded in accordance with loading
windows contained in CSM/LM Spacecraft Operational Data Book, Volume I,
Part 2, SNA-8-D-027(1) P2.
SNA-8-D-027(III)REV 2
3.5-72