Interior Right Half

The ascent stage engine compartment is formed by two beams running across the lower midsection deck and mated to the fore and aft bulkheads. Systems located in the midsection include the LM guidance computer, the power and servo assembly, ascent engine propellant tanks, RCS pro-pellant tanks, the environmental control system, and the waste management section. A tunnel ring atop the ascent stage meshes with the command module latch assemblies. During docking, the ring and clamps are aligned by...

Translunar Velocity Profile

TLI 20 SEC LOCAL HORIZONTAL ORBIT RATE TLI 15 MIN MANEUVER TO A SEPARATION ATTITUDE TLI 25 MIN SC INITIAL SEPARATION 1 EPS TLI 20 SEC LOCAL HORIZONTAL ORBIT RATE TLI 25 MIN SC INITIAL SEPARATION 1 EPS TLJ 27 MfN NULL SEPARATION RATE AND PITCH TO DOCKING ATTITUDE TLJ 27 MfN NULL SEPARATION RATE AND PITCH TO DOCKING ATTITUDE Up to four midcourse correction burns are planned during the translunar coast phase, depending upon the accuracy of the trajectory resulting from the TLI maneuver. If...

Apollo Docking Mechanisms

Rendezvous Radar

Servlce Module SM Structure The service module 1p a cylinder 12 feet 10 inches in diameter by 24 feet- 7 Inches high. For the Apollo 10 mission, It will weigh, 51,371 pounds at launch. Aluminum honeycomb panels one inch thick foim the outer skin, and milled aluminum radial beams separate the interior into six sections containing service propulsion system and reaction control fuel-oxldizer tankage, fuel cells, cryogenic oxygen and hydrogen, and onboard consumables. Spacecraft LM Adapter SLA...

Earth Reentry And Landing

Maurer Model 220g 70mm Sequence Camera

I OWN HMCH IMP P l tO LM I M LMStATUS CHECK, RECEIVE and Stow equip f LU 5-E4N VV ' COMM TES-T I IVt TO CSM IMP ANO COR IVT TO LM L 1 ACTIVATE EPS ANO S-BAND OMNJ ACTIVATE PGhKS A MO ECS JS-ftAND i-TttiASlE CHfCJCS 1 ERASABLE UEMOW DUmP I DOCKED IMU AttGN ACTIVATE ASCiNT BATTERY I PGA AND CABIN PftEttUJlE CHECKS ACTIVATE ANO INITIALIZE AOS RCS AND Hi CHECK I AGS CALIBKAUONAND ALIGN I DPS PRESSURE AT ION AND CHECKOUT 10 iOY LANOlf o' CfM J IM ANO VHF RANGING CHECKS IMU AOT REAIIGN-P5Z Ildg radar...