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Sea Dragon-2 engine
Aerojet LOx/LH2 rocket engine. Design, 1962. Truax pressure fed design. Diameter of extended nozzle 30 m. Specific impulse estimated from booster performance figures.

AKA: Sea Dragon-2. Status: Design, 1962. Thrust: 62,270.00 kN (13,998,850 lbf). Specific impulse: 320 s. Burn time: 260 s.



Country: USA. Propellants: Lox/LH2. Stages: Sea Dragon-2. Agency: Aerojet.

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