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.