Rocketdyne S-3D

http://dbpedia.org/resource/Rocketdyne_S-3D an entity of type: Software

The Rocketdyne S-3D is an American liquid rocket engine produced by Rocketdyne between 1956 and 1961 for use on the PGM-19 Jupiter and PGM-17 Thor missiles, and the Juno II rocket. Its design was used later as the basis for the H-1 rocket engine of the Saturn I, and the Rolls-Royce RZ.2 of the Blue Streak. It belongs to the LR79 engine family. rdf:langString

rdfs:label

rdf:langString Rocketdyne S-3D

rdf:langString S-3D (motor de foguete)

dbpprop:name

rdf:langString S-3D

dbpedia-owl:wikiPageID

xsd:integer 48992231

dbpedia-owl:wikiPageRevisionID

xsd:integer 1084022644

dbpprop:thrust(sl)_

xsd:integer 134908

dbpprop:combustionChamber

xsd:integer 1

dbpprop:countryOfOrigin

rdf:langString United States

dbpprop:status

rdf:langString Retired

dbpprop:type

rdf:langString liquid

dbpedia-owl:abstract

rdf:langString The Rocketdyne S-3D is an American liquid rocket engine produced by Rocketdyne between 1956 and 1961 for use on the PGM-19 Jupiter and PGM-17 Thor missiles, and the Juno II rocket. Its design was used later as the basis for the H-1 rocket engine of the Saturn I, and the Rolls-Royce RZ.2 of the Blue Streak. It belongs to the LR79 engine family.

dbpedia-owl:wikiPageLength

xsd:nonNegativeInteger 2008

rdf:type

dbpedia-owl:Software

dcterms:subject

dbpedia:Category:Rocket_engines_of_the_United_States

dbpedia:Category:Rocket_engines_using_the_gas-generator_cycle

dbpedia:Category:Rocketdyne_engines

dbpedia-owl:wikiPageWikiLink

dbpedia:Rocketdyne_H-1

dbpedia:Rolls-Royce_RZ.2

dbpedia:Saturn_I