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MISSION J-2 MASS PROPERTY DATA TABLES
Amendment 114
9/15/71
Table 3.2-20 presents the CSM-ll3/LM-ll(docked) mass properties, in Apollo
coordinates, as a function of spacecraft weight for L.O.I.
SM/SPS burn.
Table 3.2-21 presents the CSM-ll3/LM-ll(docked) mass properties, in Apollo
courdinates, as a function of spacecraft weight for the D.O.I.
SM/SPS burn.
Table 3.2-22 presents the CSM-II3 mass properties, in Apollo coordinates,
as a function of CSM weight for the Circularization I SM/SPS
burn.
Table 3.2-23 presents the CSM-II3 mass properties, in Apollo coordinates,
as a function of CSM weight for the Plane Change I SM/SPS
burn.
Table 3.2-24 presents the CSM-II3 mass properties, in Apollo coordinates
as a function of CSM weight for the T.E.I. SM/SPS burn.
Table 3.2-25 presents the LM-II mass properties, in LM coordinates, as a
function of LM weight for the P.D.I. DPS burn.
Table 3.2-26 presents the LM-ll ascent stage mass properties, in LM coordi-
nates, as a function of weight for the lunar liftoff APS burn.
Table 3.2-27 presents the LM-ll mass properties, in LM coordinates, as a
function of Lr'weight for the T.P.I. to docking LM/APS burn.
3.2-112
SNA-8-D-027(I II)REV 3