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- RS-68 abstract "The Aerojet Rocketdyne (formerly Rocketdyne and later Pratt & Whitney Rocketdyne) RS-68 (Rocket System 68) is a liquid-fuel rocket engine that uses liquid hydrogen (LH2) and liquid oxygen (LOX) as propellants in a gas-generator power cycle. It is the largest hydrogen-fueled rocket engine.Its development started in the 1990s with the goal of producing a simpler, less-costly, heavy-lift engine for the Delta IV launch system. The engine has three versions: the original RS-68, the improved RS-68A, and the RS-68B for NASA.".
- RS-68 thumbnail RS-68_rocket_engine_test.jpg?width=300.
- RS-68 wikiPageExternalLink rs68.htm.
- RS-68 wikiPageExternalLink RS-68.
- RS-68 wikiPageExternalLink PropulsionForThe21stCentury-RS-68.doc.
- RS-68 wikiPageID "1072533".
- RS-68 wikiPageRevisionID "603588784".
- RS-68 caption "An RS-68 engine undergoing hot-fire testing at NASA's Stennis Space Center during its developmental phase.".
- RS-68 chamberPressure "1488".
- RS-68 countryOfOrigin United_States.
- RS-68 cycle Gas-generator_cycle.
- RS-68 diameter "2.43 m".
- RS-68 dryWeight "14560.0".
- RS-68 firstFlight "2002".
- RS-68 fuel Liquid_hydrogen.
- RS-68 imageSize "300".
- RS-68 length "5.20 m".
- RS-68 manufacturer Rocketdyne.
- RS-68 manufacturer "Aerojet Rocketdyne".
- RS-68 manufacturer "Pratt & Whitney Rocketdyne".
- RS-68 name "RS-68".
- RS-68 nozzleRatio "21.5".
- RS-68 oxidiser Liquid_oxygen.
- RS-68 purpose "first stage engine for Delta IV rocket".
- RS-68 status "active".
- RS-68 thrust(vac)_ "758000".
- RS-68 type "liquid".
- RS-68 usedIn Delta_IV.
- RS-68 subject Category:Hydrogen_rocket_engines.
- RS-68 subject Category:Rocket_engines.
- RS-68 subject Category:Rocketdyne_engines.
- RS-68 comment "The Aerojet Rocketdyne (formerly Rocketdyne and later Pratt & Whitney Rocketdyne) RS-68 (Rocket System 68) is a liquid-fuel rocket engine that uses liquid hydrogen (LH2) and liquid oxygen (LOX) as propellants in a gas-generator power cycle. It is the largest hydrogen-fueled rocket engine.Its development started in the 1990s with the goal of producing a simpler, less-costly, heavy-lift engine for the Delta IV launch system.".
- RS-68 label "RS-68 (motor de cohete)".
- RS-68 label "RS-68 (motor de foguete)".
- RS-68 label "RS-68 (ロケットエンジン)".
- RS-68 label "RS-68".
- RS-68 label "RS-68".
- RS-68 label "RS-68".
- RS-68 label "RS-68".
- RS-68 label "RS-68".
- RS-68 label "RS-68火箭发动机".
- RS-68 sameAs RS-68.
- RS-68 sameAs RS-68.
- RS-68 sameAs RS-68_(motor_de_cohete).
- RS-68 sameAs RS-68.
- RS-68 sameAs RS-68.
- RS-68 sameAs RS-68_(ロケットエンジン).
- RS-68 sameAs RS-68.
- RS-68 sameAs RS-68_(motor_de_foguete).
- RS-68 sameAs m.043jfp.
- RS-68 sameAs Q968432.
- RS-68 sameAs Q968432.
- RS-68 wasDerivedFrom RS-68?oldid=603588784.
- RS-68 depiction RS-68_rocket_engine_test.jpg.
- RS-68 isPrimaryTopicOf RS-68.