RL-10C-X

Engine · USA

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

Pratt and Whitney LOx/LH2 rocket engine. Design concept 1994.

Engine: 317 kg (700 lb). Chamber Pressure: 102.00 bar. Area Ratio: 190. Thrust to Weight Ratio: 50. Coefficient of Thrust vacuum: 1.12.

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