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- RS-27 abstract "The RS-27 is a liquid-propellant rocket engine developed by Rocketdyne. It was used to power the first stage of the Delta 2000, 3000, 5000, and the first model of the Delta II, the Delta 6000. The RS-27 was a modified Rocketdyne H-1 from surplus engines built to power the first stage of the Saturn I and Saturn IB and replaced the MB-3 engine that had been used on previous versions of the Delta launcher. In addition to its main engine, the RS-27 included two vernier engines to provide vehicle roll control during flight.".
- RS-27 wikiPageID "45580841".
- RS-27 wikiPageLength "2198".
- RS-27 wikiPageOutDegree "23".
- RS-27 wikiPageRevisionID "651597550".
- RS-27 wikiPageWikiLink Booster_(rocketry).
- RS-27 wikiPageWikiLink Category:Rocket_engines.
- RS-27 wikiPageWikiLink Category:Rocketdyne_engines.
- RS-27 wikiPageWikiLink Delta_(rocket_family).
- RS-27 wikiPageWikiLink Delta_2000.
- RS-27 wikiPageWikiLink Delta_II.
- RS-27 wikiPageWikiLink First_stage_(rocketry).
- RS-27 wikiPageWikiLink Gas-generator_cycle.
- RS-27 wikiPageWikiLink Gas-generator_cycle_(rocket).
- RS-27 wikiPageWikiLink LOX.
- RS-27 wikiPageWikiLink Liquid-propellant_rocket.
- RS-27 wikiPageWikiLink Liquid_oxygen.
- RS-27 wikiPageWikiLink Multistage_rocket.
- RS-27 wikiPageWikiLink RP-1.
- RS-27 wikiPageWikiLink RS-27A.
- RS-27 wikiPageWikiLink Rocketdyne.
- RS-27 wikiPageWikiLink Rocketdyne_H-1.
- RS-27 wikiPageWikiLink Saturn_I.
- RS-27 wikiPageWikiLink Saturn_IB.
- RS-27 wikiPageWikiLink USA.
- RS-27 wikiPageWikiLink United_States.
- RS-27 wikiPageWikiLink Vernier_thruster.
- RS-27 wikiPageWikiLinkText "RS-27".
- RS-27 burnTime "274.0".
- RS-27 combustionChamber "1".
- RS-27 countryOfOrigin USA.
- RS-27 countryOfOrigin United_States.
- RS-27 cycle Gas-generator_cycle.
- RS-27 cycle Gas-generator_cycle_(rocket).
- RS-27 date "1974".
- RS-27 designer Rocketdyne.
- RS-27 diameter "1.07 m".
- RS-27 fuel RP-1.
- RS-27 hasPhotoCollection RS-27.
- RS-27 manufacturer Rocketdyne.
- RS-27 name "RS-27".
- RS-27 oxidiser LOX.
- RS-27 oxidiser Liquid_oxygen.
- RS-27 predecessor Rocketdyne_H-1.
- RS-27 purpose Booster_(rocketry).
- RS-27 status "Retired".
- RS-27 successor RS-27A.
- RS-27 type "liquid".
- RS-27 usedIn "Delta 2000, 3000, 5000, 6000, first stage".
- RS-27 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RS-27 wikiPageUsesTemplate Template:Reflist.
- RS-27 wikiPageUsesTemplate Template:Rocket_Engines.
- RS-27 wikiPageUsesTemplate Template:Space-stub.
- RS-27 subject Category:Rocket_engines.
- RS-27 subject Category:Rocketdyne_engines.
- RS-27 hypernym Engine.
- RS-27 type Software.
- RS-27 comment "The RS-27 is a liquid-propellant rocket engine developed by Rocketdyne. It was used to power the first stage of the Delta 2000, 3000, 5000, and the first model of the Delta II, the Delta 6000. The RS-27 was a modified Rocketdyne H-1 from surplus engines built to power the first stage of the Saturn I and Saturn IB and replaced the MB-3 engine that had been used on previous versions of the Delta launcher.".
- RS-27 label "RS-27".
- RS-27 sameAs RS-27.
- RS-27 sameAs RS-27.
- RS-27 sameAs m.012zcpqs.
- RS-27 sameAs Q11241287.
- RS-27 sameAs Q11241287.
- RS-27 wasDerivedFrom RS-27?oldid=651597550.
- RS-27 isPrimaryTopicOf RS-27.