Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Rocketdyne_H-1> ?p ?o }
- Rocketdyne_H-1 usedIn Saturn_IB.
- Rocketdyne_H-1 wikiPageUsesTemplate Template:Cite_book.
- Rocketdyne_H-1 wikiPageUsesTemplate Template:Convert.
- Rocketdyne_H-1 wikiPageUsesTemplate Template:Include-NASA.
- Rocketdyne_H-1 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Rocketdyne_H-1 wikiPageUsesTemplate Template:Reflist.
- Rocketdyne_H-1 wikiPageUsesTemplate Template:Rocket_Engines.
- Rocketdyne_H-1 wikiPageUsesTemplate Template:Sfn.
- 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 hypernym Lbf.
- Rocketdyne_H-1 type Article.
- Rocketdyne_H-1 type Company.
- Rocketdyne_H-1 type Article.
- Rocketdyne_H-1 type Company.
- Rocketdyne_H-1 type Source.
- Rocketdyne_H-1 comment "The Rocketdyne 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-I and S-IB first stages of the Saturn I and Saturn IB rockets, respectively, 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 "Rocketdyne H-1".
- Rocketdyne_H-1 sameAs H-1.
- Rocketdyne_H-1 sameAs H-1_(moteur-fusée).
- Rocketdyne_H-1 sameAs H-1_(motor_foguete).
- Rocketdyne_H-1 sameAs H-1.
- 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 Rocketdyne_H-1.
- Rocketdyne_H-1 sameAs Q1093806.
- Rocketdyne_H-1 sameAs Q1093806.
- Rocketdyne_H-1 sameAs H-1火箭发动机.
- Rocketdyne_H-1 wasDerivedFrom Rocketdyne_H-1?oldid=679526250.
- Rocketdyne_H-1 depiction H-1_rocket_engine_diagram_image.jpg.
- Rocketdyne_H-1 isPrimaryTopicOf Rocketdyne_H-1.