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Amendment 79
3130170
TABLE 3.3-14
Command Module RCS Loading Parameters and Calculations
This table will be completed when loading is accomplished. For Mission
Planning, reference should be made to Section 4.2 for nominal load, loading
tolerances, trapped and deliverable propellants.
A. Tank Volume @ 0.0 PSIA (in 3)
B. Liquid Line Volume (in 3)
C. Total A + B (in 3)
D. Initial Weight in Bleed Unit
Prior to Loading (Ib)
E°
F°
G,
H.
I.
J°
FUEL OXIDIZER
K°
L.
Tank A Tank B Tank A
1472.8 1474.7 1789.2
21.0 17.4 17.1
1493.8 1492.1 1806.3
148.6 103.3 196.6
104.4 59.1 118.3
44.2 44.2 78.3
44.2 44.6 77.8
70.0 70_0 69.0
44.2 44.2 78.3
Tank B
1787.0
16.4
1803.4
116.7
38.4
78.3
78.5
69.0
78.3
Final Weight in Bleed Unit
After Loading (ib)
Propellant Load (item D less
than E Weigh Tank)
Propellant Load by P.V.
Loading Temperature ("F)
Specification Propellant
Load @ 70_5"F (Ib)
Total CM/RCS Propellant
Load from Item G above (ib)
88.8
156.3
23.1
133.2
Maximum Trapped Propellant (Ib) 13.3
Nominal Deliverable (Ib)
75.5
3.3-55 SNA-8-D-O27(III)REV 2
ILl 111 I_ L: L E E L L E 1_ E _ |; E E L L _ L