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SE-9-3
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SE-9-3 / SE-9-5
Credit: Boeing / Rocketdyne Rocketdyne N2O4/Aerozine-50 rocket engine. Titan III Transtage. Pressure-fed. System included two modules of three engines plus two additional SE-9-5 separate engines, tanks, and a pressurization system. First flight 1964.
Date: 1964. Thrust: 107 N (24 lbf). Specific impulse: 295 s.
Family: Storable liquid. Country: USA. Propellants: N2O4/Aerozine-50. 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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