Engine Model: RS-34. Manufacturer Name: RS-34. Designer: Rocketdyne. Developed in: 1978. Propellants: N2O4/MMH. Thrust(vac): 11.700 kN (2,630 lbf). Isp: 308 sec. Country: USA. First Flight: 1983. Peacekeeper Postboost Axial Thrust. Pressure-fed. 1 main axial thruster per postboost propulsion system.
RS-34 used on Rocket Stages
