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- Reaction_Motors_XLR11 abstract "The XLR11, company designation RMI 6000C4, was the first liquid-propellant rocket engine developed in the United States for use in aircraft. It was designed and built by Reaction Motors Inc., and used ethyl alcohol and liquid oxygen as propellants to generate a maximum thrust of 6,000 lbf (27 kN). Each of the four combustion chambers produced 1,500 lbf (6.7 kN) of thrust. The engine was not throttleable but each chamber could be turned on and off individually.".
- Reaction_Motors_XLR11 thumbnail XLR-11.jpg?width=300.
- Reaction_Motors_XLR11 wikiPageExternalLink AFD-080124-094.pdf.
- Reaction_Motors_XLR11 wikiPageExternalLink EC96-43611-1.html.
- Reaction_Motors_XLR11 wikiPageExternalLink factsheet.asp?id=889.
- Reaction_Motors_XLR11 wikiPageID "542901".
- Reaction_Motors_XLR11 wikiPageLength "3860".
- Reaction_Motors_XLR11 wikiPageOutDegree "28".
- Reaction_Motors_XLR11 wikiPageRevisionID "671915981".
- Reaction_Motors_XLR11 wikiPageWikiLink Armstrong_Flight_Research_Center.
- Reaction_Motors_XLR11 wikiPageWikiLink Bell_X-1.
- Reaction_Motors_XLR11 wikiPageWikiLink Category:Aircraft_rocket_engines.
- Reaction_Motors_XLR11 wikiPageWikiLink Combustion_chamber.
- Reaction_Motors_XLR11 wikiPageWikiLink Douglas_D-558-2_Skyrocket.
- Reaction_Motors_XLR11 wikiPageWikiLink Douglas_Skyrocket.
- Reaction_Motors_XLR11 wikiPageWikiLink Dryden_Flight_Research_Center.
- Reaction_Motors_XLR11 wikiPageWikiLink Ethanol.
- Reaction_Motors_XLR11 wikiPageWikiLink Lifting_body.
- Reaction_Motors_XLR11 wikiPageWikiLink Liquid-propellant_rocket.
- Reaction_Motors_XLR11 wikiPageWikiLink Liquid_oxygen.
- Reaction_Motors_XLR11 wikiPageWikiLink Martin_Marietta_X-24A.
- Reaction_Motors_XLR11 wikiPageWikiLink Martin_Marietta_X-24B.
- Reaction_Motors_XLR11 wikiPageWikiLink National_Air_and_Space_Museum.
- Reaction_Motors_XLR11 wikiPageWikiLink National_Museum_of_the_United_States_Air_Force.
- Reaction_Motors_XLR11 wikiPageWikiLink North_American_X-15.
- Reaction_Motors_XLR11 wikiPageWikiLink Northrop_HL-10.
- Reaction_Motors_XLR11 wikiPageWikiLink Northrop_M2-F2.
- Reaction_Motors_XLR11 wikiPageWikiLink Northrop_M2-F3.
- Reaction_Motors_XLR11 wikiPageWikiLink Reaction_Motors.
- Reaction_Motors_XLR11 wikiPageWikiLink Reaction_Motors_XLR99.
- Reaction_Motors_XLR11 wikiPageWikiLink Republic_XF-91_Thunderceptor.
- Reaction_Motors_XLR11 wikiPageWikiLink Speed_of_sound.
- Reaction_Motors_XLR11 wikiPageWikiLink Throttle.
- Reaction_Motors_XLR11 wikiPageWikiLink Thrust.
- Reaction_Motors_XLR11 wikiPageWikiLink United_States.
- Reaction_Motors_XLR11 wikiPageWikiLinkText "Reaction Motors XLR11".
- Reaction_Motors_XLR11 wikiPageWikiLinkText "Reaction Motors XLR11-RM-9".
- Reaction_Motors_XLR11 wikiPageWikiLinkText "XLR 11-RM-5".
- Reaction_Motors_XLR11 caption "XLR11 rocket engine on display at the National Air and Space Museum".
- Reaction_Motors_XLR11 countryOfOrigin United_States.
- Reaction_Motors_XLR11 date "1947".
- Reaction_Motors_XLR11 fuel Ethanol.
- Reaction_Motors_XLR11 hasPhotoCollection Reaction_Motors_XLR11.
- Reaction_Motors_XLR11 imageSize "200".
- Reaction_Motors_XLR11 manufacturer Reaction_Motors.
- Reaction_Motors_XLR11 name "XLR11".
- Reaction_Motors_XLR11 oxidizer Liquid_oxygen.
- Reaction_Motors_XLR11 successor Reaction_Motors_XLR99.
- Reaction_Motors_XLR11 type "liquid".
- Reaction_Motors_XLR11 wikiPageUsesTemplate Template:Aviation_rocket_engines.
- Reaction_Motors_XLR11 wikiPageUsesTemplate Template:Convert.
- Reaction_Motors_XLR11 wikiPageUsesTemplate Template:Distinguish.
- Reaction_Motors_XLR11 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Reaction_Motors_XLR11 wikiPageUsesTemplate Template:Reflist.
- Reaction_Motors_XLR11 subject Category:Aircraft_rocket_engines.
- Reaction_Motors_XLR11 hypernym Engine.
- Reaction_Motors_XLR11 type Software.
- Reaction_Motors_XLR11 type Thing.
- Reaction_Motors_XLR11 comment "The XLR11, company designation RMI 6000C4, was the first liquid-propellant rocket engine developed in the United States for use in aircraft. It was designed and built by Reaction Motors Inc., and used ethyl alcohol and liquid oxygen as propellants to generate a maximum thrust of 6,000 lbf (27 kN). Each of the four combustion chambers produced 1,500 lbf (6.7 kN) of thrust. The engine was not throttleable but each chamber could be turned on and off individually.".
- Reaction_Motors_XLR11 label "Reaction Motors XLR11".
- Reaction_Motors_XLR11 differentFrom XLR-11_(drug).
- Reaction_Motors_XLR11 sameAs Reaction_Motors_XLR-11.
- Reaction_Motors_XLR11 sameAs Reaction_Motors_XLR11.
- Reaction_Motors_XLR11 sameAs Reaction_Motors_XLR-11.
- Reaction_Motors_XLR11 sameAs XLR11.
- Reaction_Motors_XLR11 sameAs Reaction_Motors_XLR11.
- Reaction_Motors_XLR11 sameAs m.02nc08.
- Reaction_Motors_XLR11 sameAs Q504411.
- Reaction_Motors_XLR11 sameAs Q504411.
- Reaction_Motors_XLR11 wasDerivedFrom Reaction_Motors_XLR11?oldid=671915981.
- Reaction_Motors_XLR11 depiction XLR-11.jpg.
- Reaction_Motors_XLR11 isPrimaryTopicOf Reaction_Motors_XLR11.