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15D25
KBMash solid rocket engine. RT-2 Stage 3. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/aluminum propellant.

Status: Out of Production. Date: 1961-1966. Thrust: 137.00 kN (30,798 lbf). Gross mass: 3,500 kg (7,700 lb). Unfuelled mass: 1,000 kg (2,200 lb). Burn time: 45 s. Height: 3.83 m (12.56 ft). Diameter: 0.98 m (3.21 ft).



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15D94 TsKB-7 solid rocket engine. RT-2P Stage 3. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 48 kgf/cm2.

Country: Russia. Launch Vehicles: RT-2. Propellants: Solid. Stages: 15D25. Agency: KBMash.

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