user manual

TO TRANSFORM:
1) LAUNCH VEHICLE TO APOLLO
XA = 4578.805 - XLV
LM DOCKING INTERFACE
X E = 312.5
XLV = 3468.555
312.5 IN.
LUNAR MODULE
XE = 0.0
XLV = 3156. 055
APOLLO
X A = 0.0
XLV -- 4578.805
1110 25 IN.
+X A
+X E
CM DOCKING INTERFACE
XA= 1110.25
Z E
Figure 2-17. Docked CSM/LM Station Reference
2-18
SNA-8-D-027(III)REV 2
L k