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- TR-107 abstract "The TR-107 is a developmental rocket engine designed by Northrop Grumman for Space Launch Initiative. Operating on LOX/RP-1 the engine was throttleable and had a thrust of 4,900 kN (1,100,000 lbf) at a chamber pressure of 17.7 megapascals (177 bar), making it one of the most powerful engines ever constructed.It was built by TRW following the successful conclusion of the TR-106 engine development program, a similar throttleable engine of about half the thrust that operating on LOX/LH2.".
- TR-107 wikiPageExternalLink sli-mainengine.pdf.
- TR-107 wikiPageExternalLink 100428main_tr107.pdf.
- TR-107 wikiPageID "36006129".
- TR-107 wikiPageRevisionID "599343570".
- TR-107 chamberPressure "177.0".
- TR-107 countryOfOrigin United_States.
- TR-107 fuel RP-1.
- TR-107 hasPhotoCollection TR-107.
- TR-107 manufacturer Northrop_Grumman.
- TR-107 name "TR-106".
- TR-107 oxidiser Liquid_oxygen.
- TR-107 purpose "low cost throttleable booster engine".
- TR-107 type "liquid".
- TR-107 subject Category:Rocket_engines.
- TR-107 comment "The TR-107 is a developmental rocket engine designed by Northrop Grumman for Space Launch Initiative. Operating on LOX/RP-1 the engine was throttleable and had a thrust of 4,900 kN (1,100,000 lbf) at a chamber pressure of 17.7 megapascals (177 bar), making it one of the most powerful engines ever constructed.It was built by TRW following the successful conclusion of the TR-106 engine development program, a similar throttleable engine of about half the thrust that operating on LOX/LH2.".
- TR-107 label "TR-107".
- TR-107 sameAs m.0jzv5dx.
- TR-107 sameAs Q7671209.
- TR-107 sameAs Q7671209.
- TR-107 wasDerivedFrom TR-107?oldid=599343570.
- TR-107 isPrimaryTopicOf TR-107.