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- TR-106 abstract "The TR-106 or Low Cost Pintle Engine (LCPE) was a developmental rocket engine designed by TRW under the Space Launch Initiative to reduce the cost of launch services and space flight. Operating on LOX/LH2 the engine had a thrust of 2892 kN, or 650,000 pounds, making it one of the most powerful engines ever constructed.".
- TR-106 thumbnail SSC_TR-106_Rocket_Engine_under_test.jpg?width=300.
- TR-106 wikiPageExternalLink pintleenginepaperaiaafinal.pdf.
- TR-106 wikiPageExternalLink sli-mainengine.pdf.
- TR-106 wikiPageID "28703336".
- TR-106 wikiPageRevisionID "606089536".
- TR-106 caption "A TRW 650K Low Cost Pintle Engine undergoes hot fire testing at SSC's E-1 test stand.".
- TR-106 countryOfOrigin United_States.
- TR-106 fuel Liquid_hydrogen.
- TR-106 hasPhotoCollection TR-106.
- TR-106 manufacturer TRW_Inc..
- TR-106 name "TR-106".
- TR-106 oxidiser Liquid_oxygen.
- TR-106 purpose "low cost throttleable booster engine".
- TR-106 type "liquid".
- TR-106 subject Category:Rocket_engines.
- TR-106 comment "The TR-106 or Low Cost Pintle Engine (LCPE) was a developmental rocket engine designed by TRW under the Space Launch Initiative to reduce the cost of launch services and space flight. Operating on LOX/LH2 the engine had a thrust of 2892 kN, or 650,000 pounds, making it one of the most powerful engines ever constructed.".
- TR-106 label "TR-106".
- TR-106 sameAs m.0cz8qx1.
- TR-106 sameAs Q17104238.
- TR-106 sameAs Q17104238.
- TR-106 wasDerivedFrom TR-106?oldid=606089536.
- TR-106 depiction SSC_TR-106_Rocket_Engine_under_test.jpg.
- TR-106 isPrimaryTopicOf TR-106.