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Sea Dragon-1
LOx/Kerosene propellant rocket stage. Truax pressure fed design. Sea level thrust shown. Thrust, chamber pressure varies during ascent. Vacuum thrust at cut-off 40 million kgf. Total mass, specific impulse estimated from booster performance figures.

Status: Study. Thrust: 356,900.00 kN (80,234,300 lbf). Gross mass: 11,600,000 kg (25,500,000 lb). Unfuelled mass: 1,300,000 kg (2,800,000 lb). Specific impulse: 290 s. Specific impulse sea level: 200 s. Burn time: 81 s. Height: 68.00 m (223.00 ft). Diameter: 21.50 m (70.50 ft). Span: 30.00 m (98.00 ft).



Country: USA. Engines: Sea Dragon-1 engine. Propellants: Lox/Kerosene.

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