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Sea Dragon-1 engine
Aerojet LOx/Kerosene rocket engine. Design, 1962. Truax pressure fed design. Thrust, chamber pressure varied during ascent.

AKA: Sea Dragon-1. Status: Design, 1962. Thrust: 356,900.00 kN (80,234,300 lbf). Specific impulse: 290 s. Specific impulse sea level: 200 s. Burn time: 81 s. Diameter: 21.50 m (70.50 ft).



Country: USA. Propellants: Lox/Kerosene. Stages: Sea Dragon-1. Agency: Aerojet.

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