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PF N204/Alumizine-2300k
Notional N2O4/Alumizine rocket engine. Study 1967. Used on Saturn LCB-Alumizine-140 launch vehicle.

Status: Study 1967. Thrust: 22,562.00 kN (5,072,139 lbf). Specific impulse: 280 s. Specific impulse sea level: 260 s. Burn time: 166 s.

Family: Storable liquid. Country: USA. Launch Vehicles: Saturn LCB-Alumizine-140. Propellants: N2O4/Alumizine. Stages: Saturn LCB-Alumizine-140 stage.
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