15D23

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15D23

KBMash solid rocket engine. RT-2 Stage 1. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/aluminum propellant. Chamber pressure 40 kgf/cm2.

Status: Out of Production. Date: 1961-1966. Thrust: 892.00 kN (200,529 lbf). Gross mass: 34,600 kg (76,200 lb). Unfuelled mass: 4,000 kg (8,800 lb). Burn time: 75 s. Height: 8.70 m (28.50 ft). Diameter: 1.84 m (6.03 ft).

Thrust (sl): 862.000 kN (193,785 lbf). Thrust (sl): 88,000 kgf.

Subtopics

15D23P TsKB-7 solid rocket engine. RT-2P Stage 1. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 56 kgf/cm2.

Country: Russia. Launch Vehicles: RT-2. Propellants: Solid. Stages: 15D23. Agency: KBMash.

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