L-5.00H

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L-5.00H

Notional LOx/LH2 rocket engine. Study 1963. Used on Nova GD-H launch vehicle.

Status: Study 1963. Thrust: 30,684.00 kN (6,898,037 lbf). Specific impulse: 428 s. Specific impulse sea level: 310 s. Burn time: 500 s.

Country: USA. Launch Vehicles: Nova GD-H. Propellants: Lox/LH2. Stages: Nova GD-H-1.

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