Nerva NTR

Engine · USA

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

DoE nuclear/LH2 rocket engine. Study 1991. Late 1980's update of 1960's Nerva design.

Engine: 8,500 kg (18,700 lb). Area Ratio: 500. Thrust to Weight Ratio: 4. Coefficient of Thrust sea level: 0.

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