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LR37

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

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.

Chamber Pressure: 20.00 bar.

Country
USA
Propellants
Lox/Gasoline