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5 mlbf
Status: Study 1963. Thrust: 41,361.00 kN (9,298,322 lbf). Specific impulse: 410 s. Specific impulse sea level: 345 s. Burn time: 246 s.
| 5 mlbf RP-4 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. |
Country: USA. Launch Vehicles: OOST, ROOST. Propellants: Lox/LH2. Stages: OOST stage, ROOST stage.
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