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Redstone engine
Redstone engine -

Credit: © Mark Wade. 10,228 bytes. 386 x 305 pixels.



Designer: Rocketdyne. Used on stages: Redstone. Used on launch vehicles: Redstone. Propellants: Lox/Alcohol Thrust(vac): 42,251 kgf. Thrust(vac): 414.30 kN. Isp: 265 sec. Isp (sea level): 235 sec. Burn time: 155 sec. Mass Engine: 658 kg. Diameter: 1.8 m. Chambers: 1. Country: USA. Status: Out of Production. First Flight: 1960. Last Flight: 1967. Flown: 16.
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Last update 12 March 2001.
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© Mark Wade, 2001 .