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- RL10 abstract "The RL10 is a liquid-fuel cryogenic rocket engine used on the Centaur, S-IV and DCSS upper stages. Built in the United States by Aerojet Rocketdyne (formerly by Pratt & Whitney Rocketdyne), the RL10 burns cryogenic liquid hydrogen & liquid oxygen propellants, with each engine producing 64.7–110 kN (14,545–24,729 lbf) of thrust in vacuum depending on the version in use. The RL10 was the first liquid hydrogen rocket engine to be built in the United States, and development of the engine by Marshall Space Flight Center and Pratt & Whitney began in the 1950s, with the first flight occurring in 1961. Several versions of the engine have been flown, with two, the RL10A-4-2 and the RL10B-2, still being produced and flown on the Atlas V and Delta IV.The engine produces a specific impulse (Isp) of 373–470 s (3.66–4.61 km/s) in a vacuum and has a mass ranging from 131–317 kg (289–699 lb) (depending on version). Six RL10A-3 engines were used in the S-IV second stage of the Saturn I rocket, one or two RL10 engines are used in the Centaur upper stages of Atlas and Titan rockets and one RL10B-2 is used in the upper stage of Delta IV rockets.".
- RL10 thumbnail RL-10_with_cutaway.JPG?width=300.
- RL10 wikiPageExternalLink rl10b2.htm.
- RL10 wikiPageExternalLink rl10_specs.shtml.
- RL10 wikiPageExternalLink 16rl10valve.
- RL10 wikiPageExternalLink 26altair.
- RL10 wikiPageID "713685".
- RL10 wikiPageRevisionID "605962043".
- RL10 associated Atlas_(rocket_family).
- RL10 associated Delta_IV.
- RL10 associated Saturn_I.
- RL10 associated Titan_(rocket_family).
- RL10 burnTime "700.0".
- RL10 caption "An RL10 at the U.S. Space & Rocket Center with cutaway showing tubing through the bell.".
- RL10 countryOfOrigin United_States.
- RL10 cycle Expander_cycle.
- RL10 designer Marshall_Space_Flight_Center.
- RL10 designer Pratt_&_Whitney.
- RL10 firstDate "1962".
- RL10 fuel Liquid_hydrogen.
- RL10 hasPhotoCollection RL10.
- RL10 imageSize "250".
- RL10 manufacturer Aerojet_Rocketdyne.
- RL10 manufacturer Pratt_&_Whitney_Rocketdyne.
- RL10 manufacturer "Pratt & Whitney Space Propulsion".
- RL10 mixtureRatio "5.5".
- RL10 name "RL10".
- RL10 notes "Performance values and dimensions are for RL-10B-2.".
- RL10 nozzleRatio "84".
- RL10 oxidiser Liquid_oxygen.
- RL10 purpose "Upper stage engine".
- RL10 status "In production".
- RL10 type "liquid".
- RL10 usedIn Centaur_(rocket_stage).
- RL10 usedIn Delta_Cryogenic_Second_Stage.
- RL10 usedIn S-IV.
- RL10 subject Category:Hydrogen_rocket_engines.
- RL10 subject Category:North_American_Aviation.
- RL10 subject Category:Rocket_engines.
- RL10 subject Category:Spacecraft_propulsion.
- RL10 comment "The RL10 is a liquid-fuel cryogenic rocket engine used on the Centaur, S-IV and DCSS upper stages. Built in the United States by Aerojet Rocketdyne (formerly by Pratt & Whitney Rocketdyne), the RL10 burns cryogenic liquid hydrogen & liquid oxygen propellants, with each engine producing 64.7–110 kN (14,545–24,729 lbf) of thrust in vacuum depending on the version in use.".
- RL10 label "RL-10 (moteur-fusée)".
- RL10 label "RL-10 (motor de foguete)".
- RL10 label "RL-10".
- RL10 label "RL-10".
- RL10 label "RL-10".
- RL10 label "RL10".
- RL10 label "RL10火箭发动机".
- RL10 sameAs RL-10.
- RL10 sameAs RL-10.
- RL10 sameAs RL-10_(moteur-fusée).
- RL10 sameAs RL10.
- RL10 sameAs RL-10.
- RL10 sameAs RL-10_(motor_de_foguete).
- RL10 sameAs m.0351y6.
- RL10 sameAs Q967724.
- RL10 sameAs Q967724.
- RL10 wasDerivedFrom RL10?oldid=605962043.
- RL10 depiction RL-10_with_cutaway.JPG.
- RL10 isPrimaryTopicOf RL10.