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15D24P

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15D24P
Part of 15D24 Family
TsKB-7 solid rocket engine. RT-2P Stage 2. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 48 kgf/cm2.
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Status: Out of Production. Date: 1968-1972. Thrust: 437.30 kN (98,309 lbf). Gross mass: 11,280 kg (24,860 lb). Unfuelled mass: 1,500 kg (3,300 lb). Burn time: 61 s. Height: 5.08 m (16.66 ft). Diameter: 1.49 m (4.88 ft).

Country: Russia. Launch Vehicles: RT-2P. Propellants: Solid. Agency: TsKB-7.

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