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OCR: Rendezvous Alignment radar antenna opticai lescope Inertia S-band steeraole Environmental control measurind unit anterna System module Crew compartment Docking tunnel ASCENT Crewman 10 VHF anterna STAGE [light position Aft cqui ipment bay Crewman sitting enaine cover Gaseous oxygen tan<s2 S~band inflight Reaction contro anterna locatios thruster assembly 4 locations Ascent propuision Ascent engine cover fue tank localions) Red docking Madu larized equipment stowage light assembly quadrant camera Eqress platform Fuel tank locati ons I Descent engine Oxidizer tank Iocatians) Lunar surface sensing prabe DESCENT STAGE Early Apoilo pad scientific Landing experiments pac kane quadrant LUNAR MODULE CONFIGURATION FOR INITIAL LUNAR LANDING Alignrent telescope Inertial steerable measurina moduie tun ...