15D94 (original) (raw)

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15D94

Part of 15D25

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.

Status: Out of Production. Date: 1968-1972. Number: 4 . Thrust: 180.40 kN (40,556 lbf). Gross mass: 4,640 kg (10,220 lb). Unfuelled mass: 1,040 kg (2,290 lb). Burn time: 49 s. Height: 5.45 m (17.88 ft). Diameter: 0.98 m (3.21 ft).

Country: Russia. Launch Vehicles: RT-15, RT-2P, RT-2M. Propellants: Solid. Stages: 15D94. Agency: Arsenal, TsKB-7.

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