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An F-1 engine, on loan from the National Air and Space Museum, is on display at the Air Zoo in Portage, Michigan. [22] An F-1 engine is on a horizontal display stand at Science Museum Oklahoma in Oklahoma City. [citation needed] F-1 engine F-6049 is displayed vertically at the Museum of Flight in Seattle, Washington as part of the Apollo exhibit.
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio AJ-10-190 USA: Aerojet: Space Shuttle, Orion, Apollo CSM: Active Upper N 2 O 4 /MMH: Pressure-fed: 316 [1] 26,689 [1] 8.62 [1] 118 [1] 23.08: Archimedes New ...
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The ascent propulsion system (APS) or lunar module ascent engine (LMAE) is a fixed-thrust hypergolic rocket engine developed by Bell Aerosystems for use in the Apollo Lunar Module ascent stage. It used Aerozine 50 fuel, and N
A full contract for the construction of S-IC-16 to S-IC-25 was drafted throughout mid-1967, but stages past S-IC-15 were canceled altogether in October of that year due to budgetary restrictions. [ 6 ] [ 7 ] S-IC-16 to -25 would have been utilized for follow-on Apollo missions, including those from the Apollo Applications Program .
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Apollo Guidance and control system (PDF), General Dynamics/Convair/AVCO, June 1961 GE Apollo D-2 proposal: Aerodynamics, configurations, heating, structures, and materials (PDF) , 1961 GE Feasibility Study, NASA Contract NAS 5-302: A feasibility study of an advanced manned spacecraft and system (PDF) , vol. 2 System considerations, May 15, 1961
Saturn Apollo flight profiles varied considerably by mission. [12] [13] [14] All missions began, however, with liftoff under power of the first stage. To more smoothly control engine ignition, thrust buildup and liftoff of the vehicle, restraining arms provided support and hold down at four points around the base of the S-IC stage.