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. Amendment 80
4/8/70
TABLE 3.3-10
CONSUMABLES LOADING REQUIREMENTS AND TOLERANCES
Mission H-2
SPS Propellant
Pressure _PSIA)
Fuel Oxidizer
Temperature _*F)
Fuel Oxidizer
Readout (%)
Oxidizer
quant ity
Fuel
11024 110t4 70t5 70_5 See Figure See Figure
4.1-3 4.1-4
SPS Propellant Load (Ib) Actual
iLoad
2Trapped Outside Tanks
Tanked
2Trapped Inside Tanks
3Nominal Deliverable
Loadin_ Requirement
Fuel Oxidizer
15704.0 25092.0
78.6 123.7
15625.4 24968.3
67.6 171.5
15557.8 24796.8
Fuel
15685.2
78.6
15606.6
67.6
15539.0
Oxidizer
25083.7
123.9
24960.0
171.5
24788.5
_Service Module RCS Propellant
Secondary Fuel - Quads A, B, C, D - See Loading Window - Figure 4.3-1.
Primary Fuel - Quads A, B, C, D - See Loading Window - Figure 4.3-2.
Primary and Secondary Oxidizer - Quads A, B, C, D - See Loading Window -
Figure 4.3-3.
5Co_nnand Module RCS Propellant
Fuel - System A and B - See Loading Window - Figure 4.3-4.
Oxidizer - System A and B - See Loading Window - Figure 4.3-5.
9Helium and Nitrogen
Consumable
Helium - SPS Bottles
Helium - Fuel Tanks
Helium - N20 _ Tanks
Helium - SM/RCS
Quad A
Quad B
Qued C
_ed V
Helium - _/lCS
System A
System B
Nitrogen - SM
Primary
Secondary
Pressure
(PSIA)
3600
178
178
4150
4150
4150
4150
4150
4150
2500
2500
Loadin S
Temp
('F)
70
70
70
70
70
70
70
70
70
85
85
Requirement
Weight
(lb)
87.6
5.4
6.0
1.0
1.3
Earth Launch
Weight (ib)
87.6
6.0
1.0
Actual
Pressure Temp
(PSIA) (°F)
3510
178
170
72
1.3
4350 86
4240 77
4210 73
4280 77
4140 65
4140 67
2510 71
2550 71
3.3-49
SNA-8-D-027(III)REV 2