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LH2-80k
Notional LOx/LH2 rocket engine. Study 1959. Used on Nova 4L launch vehicle.

Status: Study 1959. Thrust: 355.70 kN (79,965 lbf). Unfuelled mass: 1,438 kg (3,170 lb). Specific impulse: 425 s. Specific impulse sea level: 306 s. Burn time: 656 s.

Thrust (sl): 256.100 kN (57,574 lbf). Thrust (sl): 26,117 kgf. Engine: 1,438 kg (3,170 lb). Chamber Pressure: 30.00 bar. Area Ratio: 28. Thrust to Weight Ratio: 25.22.



Country: USA. Launch Vehicles: Nova 4L. Propellants: Lox/LH2. Stages: Nova 59-4-3, Nova 59-4-4.

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