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PF N204/UDMH-2912k
Notional N2O4/UDMH rocket engine. Study 1967. Used on Saturn LCB-Storable-140 launch vehicle.

Status: Study 1967. Thrust: 28,552.00 kN (6,418,744 lbf). Specific impulse: 267 s. Specific impulse sea level: 245 s. Burn time: 167 s.

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