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LR37
Curtiss-Wright LOx/Gasoline rocket engine. Small experimental engine for ram-rocket tests. Single thrust chamber, regeneratively cooled with gasoline, film cooling also used, spark plug ignition. Test article only built.

AKA: XLR37-CW-1. Thrust: 225 N (50 lbf). Burn time: 3,600 s. Height: 0.23 m (0.75 ft). Diameter: 0.0690 m (0.2260 ft).

Chamber Pressure: 20.00 bar.



Country: USA. Propellants: Lox/Gasoline. Agency: Curtiss-Wright.

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