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TABLE 3.i-i0
CONSUMABLES LOADING REqUIKEMENTS AND TOLERANCES
Amendment 112
7/24/71
MISSION J-i
SPS PROPELLANT
I D,es_ure (PSIA)
tuel Oxidizer
110±4 110±4
Temperature (°F)
Fuel Oxidizer
70+_5 70±5
quantity 1_ _dout (%)
Fue i Oxid ize r
See Figure See Figure
4.1-3 4.1-4
SPS Propellant Load (Ib)
]Load
2Trapped Outside Tanks
Tanked
2Trapped Inside Tanks
3Nomlnal Deliverable
Loading Requiremen, t
Fuel Oxidizer
25092.0
123.7
24968.3
171.5
24796.8
Fue I
15664.0
78.6
15585.4
67.6
15517.8
15704.0
78.6
15625.4
67.6
15557.8
Actual
Oxidizer
25035.6
123.7
24911.9
171.5
24740.4
_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.
5Command 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 Nitrosen
Consumable
Helium - SPS Bottle_
Helium - Fuel Tanks
Helium - N20 h Tanks
Helium - SM/RCS
Quads A
Quads B
Quads C
Quads D
Helium - CM/RCS
System A
System g
Nitrogen - SM
Primary
Secondary
Loadin_
Pressure
(PSIA)
3600
178
178
4150
4150
4150
4150
4150
4150
2500
2500
Te_
(°r)
70
70
70
70
70
70
70
70
70
85
85
Requl remen t
Weight
(Ib)
87.6
5.4
6.0
iJ
Actual
Earth Launch Pressure Temp
Weight (Ib)
87.6
6.0
1.0
1.3
(PSIA) (°F)
3590 87
181 74
181 72
4190 71
4200 72
4190 71
4220 72
4160 69
4110 65
2550 70
2550 70
3.1-121
SNA-8-D-027 (III) REV 3
!1 !1 I/ L l_ l: l/ L E H I,,: i U li H E L L L L