TABLE 3.5-16 (Continued)
LM-IO CONSUMABLE LOADING REQUIRE_NTS
LM-IO DPS PROPELLANT
Amendment 94*
12/10/70
Fuel (lb)
Propellant Load 7538.7
Trapped Outside Tanks 27.7
Tanked 7511.0
Trapped Inside Tanks 19.2
Nominal Deliverable 7491.8
Outage TBD
Total DPS Propellant
IEI.
2FI.
2G1.
HI.
BII.
Oxidizer (Ib)
12046.7
49.2
11997.5
40.9
11956.6
TBD
TBD
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 allow-
able tolerance for the calculated off-load is ±0.5 pounds per weigh tank.
AI. Final tank pressure at overfill (PSIG)
BI. Propellant loading temperature (°F)
Cl. Nominal overfill quantity (ib) TBD TBD
DI. Correction for tank pressure (ib)
Fuel - TBD
Oxidizer = TBD
Correction for loading temperature (ib)
Fuel - TBD
Oxidizer - TBD
Measured density (GM/CC)
Nominal density (GM/CC) 0.8994 1.4824
Delta density (GM/CC) (Item Fl-ltem GI)
Correction for measured density
Fuel - TBD
Oxidizer - TBD
Jl. Propellant in GSE
KI. Overfill quantity (CI+DI+EI+II+JI)
LI. Target loading 753g.7
M/. Quantity required to fill RCS manifolds (APS only) xxxxxxx
NI. Quantity to be off-loaded (Items KI-LI-MI)
XXXXXXX
NOTES:
ILoading temperature correction will always be negative.
2To calculate the nominal density solve the following equation where
T - temperature in °C of the measured density (usually 4°C for oxidizer
and 25°C 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)
3Correction for measured density may be either positive or negative.
3.5-80
SNA-8-D-O27(III)REV 2
t_
