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- Rocketdyne_H-1 abstract "Rocketdyne's H-1 is a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1. The H-1 was developed for use in the S-IB first stage of the Saturn I and Saturn IB rockets, where it was used in clusters of eight engines. After the Apollo program, surplus H-1 engines were rebranded and reworked as the Rocketdyne RS-27 engine with first usage on the Delta 2000 series in 1974.".
- Rocketdyne_H-1 thumbnail H-1_rocket_engine_diagram_image.jpg?width=300.
- Rocketdyne_H-1 wikiPageExternalLink 19740021163_1974021163.pdf.
- Rocketdyne_H-1 wikiPageID "713334".
- Rocketdyne_H-1 wikiPageRevisionID "606399298".
- Rocketdyne_H-1 burnTime "155.0".
- Rocketdyne_H-1 caption "A cluster of 8 H-1 rocket engines lifted the Saturn I from the launch pad.".
- Rocketdyne_H-1 chamberPressure "700".
- Rocketdyne_H-1 combustionChamber "1".
- Rocketdyne_H-1 countryOfOrigin United_States.
- Rocketdyne_H-1 cycle Gas-generator_cycle.
- Rocketdyne_H-1 date "1963".
- Rocketdyne_H-1 designer Rocketdyne.
- Rocketdyne_H-1 diameter "4.9".
- Rocketdyne_H-1 dryWeight "1000.0".
- Rocketdyne_H-1 fuel RP-1.
- Rocketdyne_H-1 hasPhotoCollection Rocketdyne_H-1.
- Rocketdyne_H-1 imageSize "150".
- Rocketdyne_H-1 length "8.8".
- Rocketdyne_H-1 manufacturer Rocketdyne.
- Rocketdyne_H-1 name "H-1".
- Rocketdyne_H-1 oxidiser Liquid_oxygen.
- Rocketdyne_H-1 purpose Booster_(rocketry).
- Rocketdyne_H-1 status "Retired".
- Rocketdyne_H-1 successor Rocketdyne_RS-27A.
- Rocketdyne_H-1 thrust(sl)_ "900 kN".
- Rocketdyne_H-1 thrustToWeight "102.47".
- Rocketdyne_H-1 type "liquid".
- Rocketdyne_H-1 usedIn Saturn_I.
- Rocketdyne_H-1 usedIn Saturn_IB.
- Rocketdyne_H-1 subject Category:Boeing.
- Rocketdyne_H-1 subject Category:North_American_Aviation.
- Rocketdyne_H-1 subject Category:Rocket_engines.
- Rocketdyne_H-1 subject Category:Rocketdyne_engines.
- Rocketdyne_H-1 comment "Rocketdyne's H-1 is a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1. The H-1 was developed for use in the S-IB first stage of the Saturn I and Saturn IB rockets, where it was used in clusters of eight engines. After the Apollo program, surplus H-1 engines were rebranded and reworked as the Rocketdyne RS-27 engine with first usage on the Delta 2000 series in 1974.".
- Rocketdyne_H-1 label "H-1 (moteur-fusée)".
- Rocketdyne_H-1 label "H-1 (motor de foguete)".
- Rocketdyne_H-1 label "H-1 (ロケットエンジン)".
- Rocketdyne_H-1 label "H-1火箭发动机".
- Rocketdyne_H-1 label "Rocketdyne H-1".
- Rocketdyne_H-1 sameAs H-1.
- Rocketdyne_H-1 sameAs H-1_(moteur-fusée).
- Rocketdyne_H-1 sameAs H-1_(mesin_roket).
- Rocketdyne_H-1 sameAs H-1_(ロケットエンジン).
- Rocketdyne_H-1 sameAs H-1_(motor_de_foguete).
- Rocketdyne_H-1 sameAs m.03513q.
- Rocketdyne_H-1 sameAs Q1093806.
- Rocketdyne_H-1 sameAs Q1093806.
- Rocketdyne_H-1 wasDerivedFrom Rocketdyne_H-1?oldid=606399298.
- Rocketdyne_H-1 depiction H-1_rocket_engine_diagram_image.jpg.
- Rocketdyne_H-1 isPrimaryTopicOf Rocketdyne_H-1.