About: AR1

An Entity of Type: Thing, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org:8891

The Aerojet Rocketdyne AR1 is a 2,200-kilonewton-class (500,000 lbf) thrust RP-1/LOX oxidizer-rich staged combustion cycle rocket engine project. The engine was conceived in 2014, and received US government funding to build a prototype engine in 2016. By 2018, the USAF had committed US$295 million of government funding to develop the engine and build an initial engine prototype, while Aerojet will put US$86 million of private capital into the project through the prototype build. As of 2019, there have been no plans to take the AR1 to full production.

Property	Value
dbo:abstract	The Aerojet Rocketdyne AR1 is a 2,200-kilonewton-class (500,000 lbf) thrust RP-1/LOX oxidizer-rich staged combustion cycle rocket engine project. The engine was conceived in 2014, and received US government funding to build a prototype engine in 2016. By 2018, the USAF had committed US$295 million of government funding to develop the engine and build an initial engine prototype, while Aerojet will put US$86 million of private capital into the project through the prototype build. As of 2019, there have been no plans to take the AR1 to full production. (en)
dbo:wikiPageExternalLink	http://www.rocket.com/innovation/ar1-engine
dbo:wikiPageID	43064873 (xsd:integer)
dbo:wikiPageLength	14287 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	1110386679 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Blue_Origin dbr:Decatur,_Alabama dbr:Huntsville,_Alabama dbr:United_Launch_Alliance dbr:NPO_Energomash dbr:BE-4 dbr:Tory_Bruno dbr:Vulcan_(rocket) dbr:Critical_Design_Review dbr:Liquid-propellant_rocket dbr:Dynetics dbr:Federal_government_of_the_United_States dbr:Firefly_Aerospace dbr:Atlas_V dbc:Rocket_engines_using_kerosene_propellant dbc:Rocket_engines_using_the_staged_combustion_cycle dbr:Aerojet_Rocketdyne dbr:Staged_combustion_cycle_(rocket) dbr:Booster_(rocketry) dbr:Methane dbr:RD-180 dbr:RD-191 dbr:RP-1 dbr:Raptor_(rocket_engine_family) dbr:LOX dbr:US_Air_Force dbr:Staged_combustion_cycle
dbp:countryOfOrigin	United States (en)
dbp:cycle	dbr:Staged_combustion_cycle_(rocket)
dbp:designer	dbr:Aerojet_Rocketdyne
dbp:fuel	dbr:RP-1
dbp:name	AR-1 (en)
dbp:oxidiser	dbr:LOX
dbp:purpose	dbr:Booster_(rocketry)
dbp:status	CDR completed, (en) not selected by ULA (en)
dbp:type	liquid (en)
dbp:wikiPageUsesTemplate	dbt:As_of dbt:Convert dbt:For dbt:Infobox_rocket_engine dbt:Reflist dbt:Short_description dbt:USD
dcterms:subject	dbc:Rocket_engines_using_kerosene_propellant dbc:Rocket_engines_using_the_staged_combustion_cycle
rdfs:comment	The Aerojet Rocketdyne AR1 is a 2,200-kilonewton-class (500,000 lbf) thrust RP-1/LOX oxidizer-rich staged combustion cycle rocket engine project. The engine was conceived in 2014, and received US government funding to build a prototype engine in 2016. By 2018, the USAF had committed US$295 million of government funding to develop the engine and build an initial engine prototype, while Aerojet will put US$86 million of private capital into the project through the prototype build. As of 2019, there have been no plans to take the AR1 to full production. (en)
rdfs:label	AR1 (en)
owl:sameAs	wikidata:AR1 https://global.dbpedia.org/id/9hGsV dbr:AR1
prov:wasDerivedFrom	wikipedia-en:AR1?oldid=1110386679&ns=0
foaf:isPrimaryTopicOf	wikipedia-en:AR1
is dbo:wikiPageRedirects of	dbr:AR-1_(rocket_engine) dbr:Aerojet_Rocketdyne_AR1 dbr:AR1_(rocket_engine)
is dbo:wikiPageWikiLink of	dbr:United_Launch_Alliance dbr:Vulcan_Centaur dbr:Firefly_Aerospace dbr:AR-1_(rocket_engine) dbr:Atlas_V dbr:RD-180 dbr:Staged_combustion_cycle dbr:Aerojet_Rocketdyne_AR1 dbr:AR1_(rocket_engine)
is foaf:primaryTopic of	wikipedia-en:AR1