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- XLR81 abstract "The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a single turbine with a gearbox to transmit power to the oxidizer and fuel pumps. The thrust chamber was all-aluminum, and regeneratively cooled by oxidizer flowing through gun-drilled passages in the combustion chamber and throat walls. The nozzle was a titanium radiatively cooled extension. The engine was mounted on an hydraulic actuated gimbal which enabled it thrust vectoring to control pitch and yaw. Engine thrust and mixture ratio were controlled by cavitating flow venturis on the gas generator flow circuit. Engine start was achieved by solid propellant start cartridge.".
- XLR81 thumbnail Agena_D_108.jpg?width=300.
- XLR81 wikiPageExternalLink msg584724.
- XLR81 wikiPageExternalLink index.htm.
- XLR81 wikiPageExternalLink msg372707.
- XLR81 wikiPageID "47013362".
- XLR81 wikiPageLength "16264".
- XLR81 wikiPageOutDegree "77".
- XLR81 wikiPageRevisionID "703954604".
- XLR81 wikiPageWikiLink Agena_target_vehicle.
- XLR81 wikiPageWikiLink Aircraft_principal_axes.
- XLR81 wikiPageWikiLink Aluminium.
- XLR81 wikiPageWikiLink Atlas-Agena.
- XLR81 wikiPageWikiLink Bell_Aircraft.
- XLR81 wikiPageWikiLink Category:Rocket_engines.
- XLR81 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- XLR81 wikiPageWikiLink Cavitation.
- XLR81 wikiPageWikiLink Combustion_chamber.
- XLR81 wikiPageWikiLink Convair_B-58_Hustler.
- XLR81 wikiPageWikiLink Dinitrogen_tetroxide.
- XLR81 wikiPageWikiLink Gas-generator_cycle.
- XLR81 wikiPageWikiLink Gemini_11.
- XLR81 wikiPageWikiLink Gimbaled_thrust.
- XLR81 wikiPageWikiLink Hydrogen_fluoride.
- XLR81 wikiPageWikiLink Hypergolic_propellant.
- XLR81 wikiPageWikiLink JP-4_(fuel).
- XLR81 wikiPageWikiLink Liquid-propellant_rocket.
- XLR81 wikiPageWikiLink Molybdenum.
- XLR81 wikiPageWikiLink Monomethylhydrazine.
- XLR81 wikiPageWikiLink Niobium.
- XLR81 wikiPageWikiLink Project_Gemini.
- XLR81 wikiPageWikiLink RM-81_Agena.
- XLR81 wikiPageWikiLink Radiative_cooling.
- XLR81 wikiPageWikiLink Red_fuming_nitric_acid.
- XLR81 wikiPageWikiLink Regenerative_cooling_(rocket).
- XLR81 wikiPageWikiLink Rocket_engine.
- XLR81 wikiPageWikiLink Rocket_engine_nozzle.
- XLR81 wikiPageWikiLink Silicone_oil.
- XLR81 wikiPageWikiLink Space_Shuttle.
- XLR81 wikiPageWikiLink Specific_impulse.
- XLR81 wikiPageWikiLink Thor-Agena.
- XLR81 wikiPageWikiLink Thorad-Agena.
- XLR81 wikiPageWikiLink Thrust_vectoring.
- XLR81 wikiPageWikiLink Titan_(rocket_family).
- XLR81 wikiPageWikiLink Titanium.
- XLR81 wikiPageWikiLink Turbopump.
- XLR81 wikiPageWikiLink United_States.
- XLR81 wikiPageWikiLink United_States_Air_Force.
- XLR81 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- XLR81 wikiPageWikiLink Venturi_effect.
- XLR81 wikiPageWikiLink File:Bell_Model_8048_Engine.jpg.
- XLR81 wikiPageWikiLinkText "XLR81".
- XLR81 associated "Thor, Thorad, Atlas and Titan".
- XLR81 burnTime "265.0".
- XLR81 caption "Standard Agena D 108 being delivered to final assembly area. Would later become Gemini Agena target vehicle 5003.".
- XLR81 combustionChamber "1".
- XLR81 countryOfOrigin "United States".
- XLR81 cycle Gas-generator_cycle.
- XLR81 date "1957".
- XLR81 firstDate "1963-07-12".
- XLR81 fuel Unsymmetrical_dimethylhydrazine.
- XLR81 gimbal "+/-2.5°".
- XLR81 lastDate "1984-04-17".
- XLR81 manufacturer Bell_Aircraft.
- XLR81 mixtureRatio "2.55".
- XLR81 name "XLR81".
- XLR81 nozzleRatio "45".
- XLR81 oxidiser Red_fuming_nitric_acid.
- XLR81 predecessor "Bell 8081".
- XLR81 purpose "upper stage engine".
- XLR81 restarts "2".
- XLR81 specificImpulseVacuum "293.0".
- XLR81 status "Retired".
- XLR81 successor "Bell 8247".
- XLR81 type "liquid".
- XLR81 usedIn RM-81_Agena.
- XLR81 wikiPageUsesTemplate Template:Atlas_rockets.
- XLR81 wikiPageUsesTemplate Template:Convert.
- XLR81 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- XLR81 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- XLR81 wikiPageUsesTemplate Template:Portal.
- XLR81 wikiPageUsesTemplate Template:Reflist.
- XLR81 wikiPageUsesTemplate Template:Rocket_Engines.
- XLR81 wikiPageUsesTemplate Template:Thor_and_Delta_rockets.
- XLR81 wikiPageUsesTemplate Template:Titan_rockets.
- XLR81 subject Category:Rocket_engines.
- XLR81 subject Category:Rocket_engines_using_hypergolic_propellant.
- XLR81 hypernym Engine.
- XLR81 type Software.
- XLR81 comment "The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a single turbine with a gearbox to transmit power to the oxidizer and fuel pumps. The thrust chamber was all-aluminum, and regeneratively cooled by oxidizer flowing through gun-drilled passages in the combustion chamber and throat walls.".
- XLR81 label "XLR81".
- XLR81 sameAs Q21449565.
- XLR81 sameAs XLR81.
- XLR81 sameAs m.013f6y27.
- XLR81 sameAs Q21449565.
- XLR81 wasDerivedFrom XLR81?oldid=703954604.
- XLR81 depiction Agena_D_108.jpg.
- XLR81 isPrimaryTopicOf XLR81.