About: RS-83

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The RS-83 was a rocket engine design for a reusable liquid hydrogen/liquid oxygen rocket larger and more powerful than any other. The RS-83 was designed to last 100 missions, and was intended for use on the first stage of a two-stage-to-orbit reusable launch vehicle.

Attributes	Values
rdf:type	yago:WikicatRocketEngines yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:Instrumentality103575240 yago:JetEngine103596285 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:Reaction-propulsionEngine104057435 yago:Rocket104099175 yago:Whole100003553
rdfs:label	RS-83 (ロケットエンジン) (ja) RS-83 (en)
rdfs:comment	The RS-83 was a rocket engine design for a reusable liquid hydrogen/liquid oxygen rocket larger and more powerful than any other. The RS-83 was designed to last 100 missions, and was intended for use on the first stage of a two-stage-to-orbit reusable launch vehicle. (en) RS-83は他のいかなるロケットよりも大きく強力な液体水素/液体酸素を推進剤とする再使用型ロケットの為に設計されたロケットエンジンである。RS-83は100回再使用が可能で二段式宇宙輸送機に搭載する予定だった。 (ja)
name	RS-83 (en)
dcterms:subject	Rocket engines of the United States Rocket engines using the gas-generator cycle Rocketdyne engines Rocket engines using hydrogen propellant
Wikipage page ID	5559342 (xsd:integer)
Wikipage revision ID	1066129350 (xsd:integer)
Link from a Wikipage to another Wikipage	Multistage rocket Human spaceflight United States LH2 Constellation program Liquid hydrogen Gas-generator cycle (rocket) Pratt & Whitney Rocketdyne Rocket engines of the United States Rocket engines using the gas-generator cycle Rocketdyne engines Liquid oxygen Reusable launch vehicle Rocket engines using hydrogen propellant Space Shuttle Main Engine RS-68 Space Launch Initiative Expendable launch system LOX Rocketdyne Rocket engine Canoga Park, California J-2 (rocket engine) RS-84 Thrust to weight ratio Delta IV rocket
Link from a Wikipage to an external page	https://web.archive.org/web/20041019022626/https:/rockettest.ssc.nasa.gov/ssc_ptd/projects_rs83.htm
sameAs	RS-83 RS-83 RS-83 RS-83 RS-83
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_rocket_engine dbt:Reflist dbt:Short_description
country of origin	United States
cycle	Gas-generator cycle (rocket)
fuel	LH2
manufacturer	Pratt & Whitney Rocketdyne
oxidiser	LOX
purpose	first stage (en)
status	prototype (en)
type	liquid (en)
has abstract	The RS-83 was a rocket engine design for a reusable liquid hydrogen/liquid oxygen rocket larger and more powerful than any other. The RS-83 was designed to last 100 missions, and was intended for use on the first stage of a two-stage-to-orbit reusable launch vehicle. (en) RS-83は他のいかなるロケットよりも大きく強力な液体水素/液体酸素を推進剤とする再使用型ロケットの為に設計されたロケットエンジンである。RS-83は100回再使用が可能で二段式宇宙輸送機に搭載する予定だった。 (ja)
designed by	Pratt & Whitney Rocketdyne
gold:hypernym	Design
prov:wasDerivedFrom	wikipedia-en:RS-83?oldid=1066129350&ns=0
page length (characters) of wiki page	3793 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:RS-83
is Link from a Wikipage to another Wikipage of	Rs-83 RS-68
is Wikipage redirect of	Rs-83
is foaf:primaryTopic of	wikipedia-en:RS-83

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