5 mlbf RP-4

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5 mlbf RP-4

Part of 5 mlbf

Notional LOx/Kerosene rocket engine. Study 1963. Operational date would have been July 1977. Recoverable stage. 10% plug nozzle. Used on Nova-1 DAC launch vehicle.

Status: Study 1963. Thrust: 24,459.00 kN (5,498,601 lbf). Specific impulse: 299 s. Specific impulse sea level: 260 s. Burn time: 118 s.

Country: USA. Launch Vehicles: Nova-1 DAC. Propellants: Lox/Kerosene. Stages: Nova DAC-1.

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