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15D24
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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.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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