Manufacturer Name: SE-5-2. Designer: Rocketdyne. Developed in: 1962. Application: SE-5-2/-3. Propellants: N2O4/UDMH. Thrust(vac): 205 N (46 lbf). Isp: 272 sec. Country: USA. First Flight: 1963.
Agena Auxiliary. Pressure-fed. SE-5-2 four engines in satellite system. SE-5-3 two engines for Agena auxiliary propuslion.