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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.
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Aerojet Rocketdyne AR1 | Application | Booster | 1.00 | infobox |
| Aerojet Rocketdyne AR1 | Country of origin | United States | 1.00 | infobox |
| Aerojet Rocketdyne AR1 | Cycle | Staged combustion | 1.00 | infobox |
| Aerojet Rocketdyne AR1 | Designer | Aerojet Rocketdyne | 1.00 | infobox |
| Aerojet Rocketdyne AR1 | Propellant | LOX / RP-1 | 1.00 | infobox |
| Aerojet Rocketdyne AR1 | Status | CDR completed, not selected by ULA | 1.00 | infobox |
| Aerojet Rocketdyne AR1 | Thrust, sea-level | 2,224 kN (500,000 lbf) | 1.00 | infobox |
| Aerojet Rocketdyne AR1 | Thrust, vacuum | 2,500 kN (560,000 lbf) | 1.00 | infobox |
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