user manual

Amendment 94
12/10/70
SUPPLEMENTARY DATA APPLICABLE TO SEQUENTIAL MASS PROPERTIES TABLES
General Comments to be applied to Tables 3.5-1 through 3.5-8:
Inertia data dispersions are +10%.
Dispersions shall be used as 3o deviation values.
All initial propellant weights are total tanked.
The (+) or (-) sign following the name of an item indicates that the
item is added to or subtracted from the preceding total.
Table 3.5-1
SM/SPS glmbal angles for SPS abort sequence are: Pitch ffi-0.4104
Yaw = 1.895
Tables 3.5-7 and 3.5-8
CSM and LM consumables changes are presented in Tables 3.5-7 and
3.5-8, respectively.
Table 3.5-3
The mass Spectrometer and Gamma-Ray Spectrometer are shown deployed
after each SPS firing following D.O.I. For all other summations the
M.S. and G.R. Spectrometers are not deployed. The following are the
individual mass properties for the M.S. and G.R. Spectrometers in
Apollo Coordinates.
Weight X-Bar Y-Bar Z-Bar
(ib) (in) (in) (in)
Gamma-Ray 45.4 865.1 33.0 -57.0
Retracted
Gamma-Ray _28.0 865.1 231,3 -312.4
Deployed _17.4 865.1 132.2 -184.7
Mass Spectrometer 47.4 863.1 55.8 -40.5
Retracted
Mass Spectrometer _27.4 863.1 341.7 -149.4
Deployed _20.0 863.1 198.8 -94.9
3.5-1
SNA-8-D-O27(III)REV 2