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LE-3
LE-3
LE-3
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/Aerozine-50 rocket engine. MHI(Japan)/Rocketdyne Upper Stage. Pressure-fed.

Date: 1970. Thrust: 53.34 kN (11,991 lbf). Specific impulse: 285 s.



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

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