Nerva 2 engine

Engine · USA

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

DoE nuclear/LH2 rocket engine. Developed 1950-74.

Thrust (sl): 399.500 kN (89,811 lbf). Thrust (sl): 40,741 kgf. Engine: 11,860 kg (26,140 lb). Thrust to Weight Ratio: 7.45792580101181.

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