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RL-10C
Part of RL-10
Pratt and Whitney LOx/LH2 rocket engine. In Production. Used in Delta 3 - 2. First flight 1998.

Status: In Production. Thrust: 155.70 kN (35,003 lbf). Unfuelled mass: 317 kg (698 lb). Specific impulse: 450 s. Burn time: 469 s. Diameter: 3.05 m (10.00 ft).

Engine: 317 kg (700 lb). Chamber Pressure: 102.00 bar. Area Ratio: 190. Thrust to Weight Ratio: 49.99.

Country: USA. Propellants: Lox/LH2. Agency: Pratt and Whitney.
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