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The Aerojet Rocketdyne AR1 is a 2,200-kilo … 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. plans to take the AR1 to full production.
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http://www.rocket.com/innovation/ar1-engine +
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14287
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United States
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http://dbpedia.org/resource/RP-1 +
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AR-1
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http://dbpedia.org/resource/LOX +
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http://dbpedia.org/resource/Booster_%28rocketry%29 +
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not selected by ULA
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liquid
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| rdfs:comment |
The Aerojet Rocketdyne AR1 is a 2,200-kilo … 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. plans to take the AR1 to full production.
|
| rdfs:label |
AR1
|
