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Credit: Boeing / Rocketdyne
Rocketdyne N2O4/Aerozine-50 rocket engine. Lunar Module Descent. Pressure-fed. Thrust throttleable 1050-10,500 lbs vac. First flight 1968.

Date: 1963. Thrust: 46.67 kN (10,492 lbf). Specific impulse: 305 s.



Family: Storable liquid. Country: USA. Propellants: N2O4/Aerozine-50. Agency: Rocketdyne.

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