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PF N204/UDMH-2165k
Notional N2O4/UDMH rocket engine. Study 1967. Used on Saturn LCB-Storable-250 launch vehicle.

Status: Study 1967. Thrust: 21,232.00 kN (4,773,143 lbf). Specific impulse: 267 s. Specific impulse sea level: 245 s. Burn time: 163 s.

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