user manual

Amendment 86
9110170
TABLE 3.5-13
SPS PItOPILL_ I/tICZlTJLINTIES
ITEM
LOADING UtiCEitSAIttTIES
Tank Volume
Tanparacure Gauss ('2.0oF)
Standpipe Helaht
Propellant Gouje (tO.35X of Oauaeable)
Density Meaeurtment (i)
Batch Density (I)
hoadlnB Pressure (I)
RSS
FUXL
(Ib)
t24
"18
• 6
"54
t 0
t9h
t8
t113
TOTAL RSS t172
Loadin$ Specification (1) (2)
Tolerance on Propellant Temperature
of Flight Load
TOTAL LOADING UNCERTAINTY
MISSION UNCERTAINTIES
Mixture Ratio Variation
iV. Iep, Vehicle Welehc Variation
Propellant usaee uncertainty due to
total loadin8 uncertainty
OXIDIZZl
(lb)
t39
it6
"10
• 86
t 0
.75
'14
'130
t16 t24
+0.0 +0.0
-46.0 -113.0
i
+212
-371
TBD
TBD
TBD
TOTAL PROPELLANT UNCERTAINTY FOI
MISSION AV TBD
NOTES: (1) Data viii be known after loadin8 is accolpliahed.
(2) Loedieql specification is an allovable tolerance about
nouinal, this number is added to the loadilqJ uncertainty
variables.
3.5-76
SNA-8-D-02 7 (III) REV 2
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