user manual

TABLE 3.4-16 (Continued)
LM-8 Consumable Loadin E Requirements
124-8 DPS Propellant
Fuel (Ib) Oxidizer (Ib)
Propellant Load 7072.8 11341.9
Trapped Outside Tanks 35.1 60.5
ranked 7037.7 11281.4
trapped Inside Tanks 14.8 102.7
Nominal Deliverable 7022.9 11178.7
Outage TBD TBD
Total DPS Propellant Available TBD
Amendment 91
11/25/70
The following table should be used to determine the amount of propellant to be
off-loaded from a full condition to arrive at the indicated load. The allowable
tolerance for the calculated off-load is_+0.5 pounds per weigh tank.
AI. Final tank pressure at overfill (PSIG)
BI. Propellant loading temperature (OF)
C1. Nominal overfill quantity (lb) 7160.4
D1. Correction for tank pressure (lb)
& Fuel = 0.31 (Item AI-40)
A Oxidizer - 0.51 (Item AI-40)
IEI. Correction for loading temperature (ib)
& Fuel = -4.0 (Item BI-65)
A Oxidizer - -9.85 (Item BI-65)
2F1. Measured density (GM/CC)
2G1. Nominal density (GM/CC) 0.8994
N1. Delta density (GM/CC) (Item Fl-Item G1)
3II. Correction for measured density
A Fuel - 7900 (Item HI)
A Oxidizer - 7900 (Item HI)
Jl. Propellant in GSE
KI. Overfill quantity (CI+DI+EI+II+J1)
LI. Target loading 7072.8
MI. Quantity required to fill RCS manifolds
(APS only) xxxxxx
NIo Quantity to be off-loaded
(Items KI-L1-M1)
11452.9
1.4824
11341.9
XXXXXX
NOTES :
ILoadln8 temperature correction will always be nesatlve.
2To calculate the nominal density solve the following equation where
T-temperature in *C of the measured density (usually 4"C for oxidizer
and 25oC for fuel). This equation is valid for 14.7 PSIA. Therefore,
the measured density must also be at 14.7 PSIA.
Nominal fuel density - 0.922904-0.0009377 (°C)
Nominal oxidizer density - 1.491539-0.0022832 (°C)
3Correcclon for measured density may be either positive or negative.
3.4-74 SNA-8-D-027(III)REV 2
!1 !1 1: I: U 1.: L L I: I: L L L: L: L L