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MISSION H-3 MASS PROPERTY DATA TABLES
Amendment H8
10/5/70
Table 3.4-20 presents CSM-II0/LM-8 (docked) mass propertieu, iu Apollo
coordinates, as a function of spacecraft weight for the
Hybrid SM/SPS burn.
Table 3.4-21 presents CSM-II0/LM-8 (docked) mass properties, in Apollo
coordinates, as a function of spacecraft weight for L.O.I.
SM/SPS burn.
Table 3.4-22 presents the CSM-II0/LM-8 (docked) mass properties, in Apollo
coordinates as a function of spacecraft weight for the
D.O.I. SM/SPS burn.
Table 3.4-23 presents the CSM-II0 mass properties, in Apollo coordinates,
as a function of CSM weight for the Circularlzatlon I Srl/SPS
burn.
Table 3.4-24 presents the CSM-II0 mass properties, in Apollo coordinates,
as a function of CSM weight for the Plane Change I SM/SPS
burn.
Table 3.4-25 presents the CSM-II0 mass properties, in Apollo coordinates,
as a function of CSM weight for the T.E.I. SM/SPS burn.
Table 3.4-26 presents the LM-8 mass properties, in LM coordinates, as a
function of LM weight for the P.D.I. DPS burn.
Table 3.4-27 presents the LM-8 ascent stage mass properties, in LM coordinates
as a function of weight for the lunar lift-off APS burn.
Table 3.4-28 presents the LM-8 mass properties, in LM coordinates, as a
function of LM weight for the T.P.I. burn.
3.4-80
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