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SE-5-2/-3
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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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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