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PF N204/Alumizine-1925k
Notional N2O4/Alumizine rocket engine. Study 1967. Used on Saturn LCB-Alumizine-250 launch vehicle.

Status: Study 1967. Thrust: 18,873.00 kN (4,242,819 lbf). Specific impulse: 280 s. Specific impulse sea level: 260 s. Burn time: 168 s.

Family: Storable liquid. Country: USA. Launch Vehicles: Saturn LCB-Alumizine-250. Propellants: N2O4/Alumizine. Stages: Saturn LCB-Alumizine-250 stage.
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