Engine Model: 15D23P. Designer: TsKB-7. Developed in: 1968-1972. Application: RT-2P Stage 1. Gross Mass: 34,550 kg (76,160 lb). Empty Mass: 3,750 kg (8,260 lb). Propellants: Solid. Thrust(vac): 980.000 kN (220,310 lbf). Burn time: 75 sec. Diameter: 1.84 m (6.03 ft). Length: 9.20 m (30.10 ft). Chambers: 1. Country: Russia. Status: Out of Production. Three gimballed nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 56 kgf/cm2.
RT-184 used on Rocket Stages
- Used on stage: 15D23. on launch vehicle: RT-2.