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Amendment 87
9115170
MISSION J-i MASS PROPERTY DATA TABLES
Table 3.5-20 presents the CSM-112/LM-lO(docked) ms properties, in Apollo
coordinates, as 8 function of spacecraft weight for L.O.I.
SM/SPS burn.
Table 3.5-21 presents the CSM-112/LM-10 (docked) mass propercles, In Apollo
coordinates, as I functio_ of spacecraft welahC for the
D.O.I. SM/SPS burn.
Table 3,5-22 presence the CSM-112 mama properties, in Apollo coordinates,
as a function of CSM weight for the Circularization I SM/SPS
burn.
Table 3.5-23 presents the CSM-112 mass properties, in Apollo coordinates,
as a function of CSM waisht for the Plane Change I SM/SPS
burn.
Table 3.5-24 presents the CSM-112 mass properties, in Apollo coordinates,
as a function of CSM wei6ht for the T.E.I. SN/SPS burn.
Table 3.5-25 presence the LM-10mas8 properties, in LM coordinates, as a
function of I/4 weiSht for the P.D.I. DPS burn.
Table 3.5-26 presents the LN-10iscent sCaBs mass properties, in I24 coordinates,
as a function, of weiiht for the lunar liftoff AFS burn.
Table 3.5-27 presents the L/f-10ums8 properties, in 124 coordinates, as a
function of LM lmisht for the T .P .I. to docking LM/RCS burn.
3.5-86 SNA-8-D-027 (III)P.EV 2
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