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- Ascent_Propulsion_System abstract "The Ascent Propulsion System (APS) or LMAE (Lunar Module Ascent Engine) 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 N2O4 oxidizer. Rocketdyne provided the injector system, at the request of NASA, when Bell could not solve combustion instability problems.".
- Ascent_Propulsion_System thumbnail Apollo_Lunar_Module_Ascent_Engine.jpg?width=300.
- Ascent_Propulsion_System wikiPageExternalLink 19730011150_1973011150.pdf.
- Ascent_Propulsion_System wikiPageExternalLink 20090016298_2009014419.pdf.
- Ascent_Propulsion_System wikiPageID "36063779".
- Ascent_Propulsion_System wikiPageLength "6635".
- Ascent_Propulsion_System wikiPageOutDegree "37".
- Ascent_Propulsion_System wikiPageRevisionID "702334755".
- Ascent_Propulsion_System wikiPageWikiLink Aerozine_50.
- Ascent_Propulsion_System wikiPageWikiLink Agena_target_vehicle.
- Ascent_Propulsion_System wikiPageWikiLink Service_Module.
- Ascent_Propulsion_System wikiPageWikiLink Apollo_Lunar_Module.
- Ascent_Propulsion_System wikiPageWikiLink Bell_Aircraft.
- Ascent_Propulsion_System wikiPageWikiLink Category:Apollo_program_hardware.
- Ascent_Propulsion_System wikiPageWikiLink Category:Rocket_engines.
- Ascent_Propulsion_System wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- Ascent_Propulsion_System wikiPageWikiLink Category:Spacecraft_propulsion.
- Ascent_Propulsion_System wikiPageWikiLink Corona_(satellite).
- Ascent_Propulsion_System wikiPageWikiLink Dinitrogen_tetroxide.
- Ascent_Propulsion_System wikiPageWikiLink Hypergolic_propellant.
- Ascent_Propulsion_System wikiPageWikiLink Lockheed_Corporation.
- Ascent_Propulsion_System wikiPageWikiLink Lunar_Orbiter_program.
- Ascent_Propulsion_System wikiPageWikiLink Missile_Defense_Alarm_System.
- Ascent_Propulsion_System wikiPageWikiLink Moon_Machines.
- Ascent_Propulsion_System wikiPageWikiLink Pratt_&_Whitney_Rocketdyne.
- Ascent_Propulsion_System wikiPageWikiLink Pressure-fed_engine.
- Ascent_Propulsion_System wikiPageWikiLink Project_Gemini.
- Ascent_Propulsion_System wikiPageWikiLink RM-81_Agena.
- Ascent_Propulsion_System wikiPageWikiLink RS-18.
- Ascent_Propulsion_System wikiPageWikiLink Ranger_program.
- Ascent_Propulsion_System wikiPageWikiLink Reconnaissance_satellite.
- Ascent_Propulsion_System wikiPageWikiLink Rocket_engine.
- Ascent_Propulsion_System wikiPageWikiLink Rocketdyne.
- Ascent_Propulsion_System wikiPageWikiLink Samos-F.
- Ascent_Propulsion_System wikiPageWikiLink Samos_(satellite).
- Ascent_Propulsion_System wikiPageWikiLink Science_(TV_network).
- Ascent_Propulsion_System wikiPageWikiLink Spacecraft.
- Ascent_Propulsion_System wikiPageWikiLink Titan_IIIB.
- Ascent_Propulsion_System wikiPageWikiLink United_States.
- Ascent_Propulsion_System wikiPageWikiLink File:Apollo_17_LM_Ascent_Stage.jpg.
- Ascent_Propulsion_System wikiPageWikiLinkText "Ascent Propulsion System".
- Ascent_Propulsion_System wikiPageWikiLinkText "LMAE".
- Ascent_Propulsion_System wikiPageWikiLinkText "Lunar Module Ascent Engine".
- Ascent_Propulsion_System wikiPageWikiLinkText "ascent rocket engine".
- Ascent_Propulsion_System wikiPageWikiLinkText "ascent rocket".
- Ascent_Propulsion_System caption "Apollo LM Ascent Engine".
- Ascent_Propulsion_System combustionChamber "1".
- Ascent_Propulsion_System cycle Pressure-fed_engine.
- Ascent_Propulsion_System date "1964".
- Ascent_Propulsion_System fuel Aerozine_50.
- Ascent_Propulsion_System imageSize "250".
- Ascent_Propulsion_System manufacturer Bell_Aircraft.
- Ascent_Propulsion_System manufacturer Rocketdyne.
- Ascent_Propulsion_System name "Ascent Propulsion System".
- Ascent_Propulsion_System oxidizer Dinitrogen_tetroxide.
- Ascent_Propulsion_System predecessor "Bell 8247".
- Ascent_Propulsion_System purpose "Lunar Ascent Stage/Spacecraft propulsion".
- Ascent_Propulsion_System status "Retired".
- Ascent_Propulsion_System successor RS-18.
- Ascent_Propulsion_System thrustToWeight "19.44".
- Ascent_Propulsion_System type "liquid".
- Ascent_Propulsion_System usedIn "Lunar Module as Ascent Engine".
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Apollo_program_hardware.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Citation_needed.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Convert.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Include-NASA.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Main.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:Reflist.
- Ascent_Propulsion_System wikiPageUsesTemplate Template:USA.
- Ascent_Propulsion_System subject Category:Apollo_program_hardware.
- Ascent_Propulsion_System subject Category:Rocket_engines.
- Ascent_Propulsion_System subject Category:Rocket_engines_using_hypergolic_propellant.
- Ascent_Propulsion_System subject Category:Spacecraft_propulsion.
- Ascent_Propulsion_System type Source.
- Ascent_Propulsion_System comment "The Ascent Propulsion System (APS) or LMAE (Lunar Module Ascent Engine) 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 N2O4 oxidizer. Rocketdyne provided the injector system, at the request of NASA, when Bell could not solve combustion instability problems.".
- Ascent_Propulsion_System label "Ascent Propulsion System".
- Ascent_Propulsion_System sameAs Q4803858.
- Ascent_Propulsion_System sameAs LMAE.
- Ascent_Propulsion_System sameAs Ascent_Propulsion_System.
- Ascent_Propulsion_System sameAs 月着陸船用上昇エンジン.
- Ascent_Propulsion_System sameAs m.0j_4ntl.
- Ascent_Propulsion_System sameAs Q4803858.
- Ascent_Propulsion_System wasDerivedFrom Ascent_Propulsion_System?oldid=702334755.
- Ascent_Propulsion_System depiction Apollo_Lunar_Module_Ascent_Engine.jpg.
- Ascent_Propulsion_System isPrimaryTopicOf Ascent_Propulsion_System.