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- RS-83 abstract "The RS-83 was a rocket engine design for a reusable liquid hydrogen/liquid oxygen rocket larger and more powerful than any other. The RS-83 was designed to last 100 missions, and was intended for use on the first stage of a two-stage-to-orbit reusable launch vehicle.".
- RS-83 wikiPageExternalLink projects_rs83.htm.
- RS-83 wikiPageID "5559342".
- RS-83 wikiPageRevisionID "571297626".
- RS-83 countryOfOrigin United_States.
- RS-83 cycle Gas-generator_cycle.
- RS-83 designedBy Pratt_&_Whitney_Rocketdyne.
- RS-83 dryWeight "12700.0".
- RS-83 fuel Liquid_hydrogen.
- RS-83 hasPhotoCollection RS-83.
- RS-83 manufacturer Pratt_&_Whitney_Rocketdyne.
- RS-83 name "RS-83".
- RS-83 oxidiser Liquid_oxygen.
- RS-83 purpose "first stage".
- RS-83 specificImpulseVacuum "446.0".
- RS-83 status "prototype".
- RS-83 thrust(vac)_ "750000".
- RS-83 type "liquid".
- RS-83 subject Category:Rocket_engines.
- RS-83 comment "The RS-83 was a rocket engine design for a reusable liquid hydrogen/liquid oxygen rocket larger and more powerful than any other. The RS-83 was designed to last 100 missions, and was intended for use on the first stage of a two-stage-to-orbit reusable launch vehicle.".
- RS-83 label "RS-83 (ロケットエンジン)".
- RS-83 label "RS-83".
- RS-83 sameAs RS-83_(ロケットエンジン).
- RS-83 sameAs m.0dsjwd.
- RS-83 sameAs Q7277682.
- RS-83 sameAs Q7277682.
- RS-83 wasDerivedFrom RS-83?oldid=571297626.
- RS-83 isPrimaryTopicOf RS-83.