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15D24P
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Designer: TsKB-7. Developed in: 1968-1972. Application: RT-2P Stage 2. Gross Mass: 11,280 kg (24,860 lb). Empty Mass: 1,500 kg (3,300 lb). Propellants: Solid. Thrust(vac): 437.300 kN (98,309 lbf). Burn time: 61 sec. Diameter: 1.49 m (4.88 ft). Length: 5.08 m (16.66 ft). Chambers: 1. Country: Russia. Status: Out of Production. Three gimballed nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 48 kgf/cm2.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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