LH2-80k

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

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

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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