user manual

TABLE 3.4-18
Amendment 98
1/22/71
LM-8 Propellant Loadins Uncertainties
LM-8 APS PROPELLANT
Vent line Volume
Tank Volume
Pressure Measurement (±5 PSIA)
Temperature Measurement (±l.5°F)
Measured Density
2Weight Measurement
lLoading Tolerance
Total Loading Uncertainty
Fuel (ib)
±0.2
±0.8
±0.5
±1.7
±0.7
±0.5
±0.0
±4.4
Oxidizer (ib)
±0.3
LM-8 DPS PROPELLANT
Vent Line Volume
Tank Volume
Pressure Measurement (±5 PSIA)
Temperature Measurement (l.5°F)
Measured Density
2Weight Measurement
ILoading Tolerance
Total Loading Uncertainty
±1.3
±0.8
±4.3
±0.5
±0.5
±0.0
±7.7
±0.2 ±0.3
±3.4 ±5.6
±1.6 ±2.6
±6.1 ±14.8
±2.4 ±i,6
±o,_ ±0,_
±0.5 ±0.5
±14.2 ±25,4
ZO.6 ±I.8
±0.4 ±0.6
zO.8 zl.4
Zl.8 ±3.8
Loading Temperature
Ullage Calculation
Tank and Manifold Volume
Total
LM-8 RCS PROPELLANT
IThese will be known quantities after loading is accompllshed.
21f weigh tank is used for off-loadlng, then weight measurement uncertainty
is ±0.5 pounds per weigh tank. If flow meter is used for off-loading, then
weight measuremnt uncertainty is ZA.0X of amount off-loadad.
3.4-96
SNA-8-D-027(III)REV 2