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NERVA/Lox Mixed Cycle
Notional nuclear/LH2 rocket engine. Study 1963. Used on RITA C launch vehicle.

Status: Study 1963. Thrust: 24,126.00 kN (5,423,740 lbf). Specific impulse: 810 s. Specific impulse sea level: 410 s. Burn time: 285 s.

Propellant Formulation: Nuclear/Lox/LH2.



Family: nuclear-powered. Country: USA. Engines: NERVA/Lox Mixed Cycle. Launch Vehicles: RITA C. Propellants: Nuclear/LH2.

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