Engine Model: 15D24. Designer: TsKB-7. Developed in: 1961-1966. Application: RT-2 Stage 2. Propellants: Solid. Thrust(vac): 431.000 kN (96,892 lbf). Burn time: 60 sec. Diameter: 1.48 m (4.85 ft). Length: 4.74 m (15.55 ft). Chambers: 1. Country: Russia. Status: Out of Production. Three gimballed nozzles for steering. Ammonium perchlorate/aluminium propellant. Chamber pressure 40 kgf/cm2. Average thrust 33 tonnes.
15D24 used on Rocket Stages
- Used on stage: 15D24. on launch vehicle: RT-2.