L-5.25H (original) (raw)

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L-5.25H

Notional LOx/LH2 rocket engine. Study 1963. Engines for recoverable booster engine package 'half stage' of a 1 1/2 stage arrangement. Used on Nova GD-H launch vehicle.

Status: Study 1963. Thrust: 27,350.00 kN (6,148,520 lbf). Specific impulse: 410 s. Specific impulse sea level: 350 s. Burn time: 190 s.

Separation at 2,980 m/s at 87,800 m altitude; splashdown under 4 46 m diameter parachutes 1,000 km downrange.

Country: USA. Launch Vehicles: Nova GD-H. Propellants: Lox/LH2. Stages: Nova GD-H-0.

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