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RL-10C
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Designer: Pratt and Whitney. Propellants: Lox/LH2. Thrust(vac): 155.700 kN (35,003 lbf). Isp: 450 sec. Burn time: 469 sec. Mass Engine: 317 kg (700 lb). Diameter: 3.05 m (10.00 ft). Chambers: 1. Chamber Pressure: 102.00 bar. Area Ratio: 190.00. Thrust to Weight Ratio: 49.99. Country: USA. Status: In Production. First Flight: 1998. Last Flight: 2000. Used in Delta 3 - 2.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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