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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 wikiPageExternalLink 19730011150_1973011150.pdf.
- Ascent_Propulsion_System wikiPageExternalLink 20090016298_2009014419.pdf.
- Ascent_Propulsion_System wikiPageID "36063779".
- Ascent_Propulsion_System wikiPageRevisionID "587045699".
- 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 hasPhotoCollection Ascent_Propulsion_System.
- 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 subject Category:Apollo_program_hardware.
- Ascent_Propulsion_System subject Category:Rocket_engines.
- 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 Ascent_Propulsion_System.
- Ascent_Propulsion_System sameAs m.0j_4ntl.
- Ascent_Propulsion_System sameAs Q4803858.
- Ascent_Propulsion_System sameAs Q4803858.
- Ascent_Propulsion_System wasDerivedFrom Ascent_Propulsion_System?oldid=587045699.
- Ascent_Propulsion_System isPrimaryTopicOf Ascent_Propulsion_System.