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SE-5-2/-3
SE-5-2/-3
SE-5-2/-3
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/UDMH rocket engine. SE-5-2/-3. Agena Auxiliary. Pressure-fed. SE-5-2 four engines in satellite system. SE-5-3 two engines for Agena auxiliary propulsion. First flight 1963.

AKA: SE-5-2. Date: 1962. Thrust: 205 N (46 lbf). Specific impulse: 272 s.

Propellant Formulation: N2O4/Hydrazine(75%)-MMH(25%).



Family: Storable liquid. Country: USA. Propellants: N2O4/UDMH. Agency: Rocketdyne.

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