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15D24
TsKB-7 solid rocket engine. RT-2 Stage 2. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/aluminum propellant. Chamber pressure 40 kgf/cm2. Average thrust 33 metric tons.

Status: Out of Production. Date: 1961-1966. Thrust: 431.00 kN (96,892 lbf). Gross mass: 9,600 kg (21,100 lb). Unfuelled mass: 1,500 kg (3,300 lb). Burn time: 60 s. Height: 4.74 m (15.55 ft). Diameter: 1.48 m (4.85 ft).

Subtopics

RD RT-15-2 OKB-1 solid rocket engine. RT-1 second stage.

15D24P 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.

15D27 Arsenal solid rocket engine.

RD RT-21-2 MITT solid rocket engine. Pioner second stage.

Country: Russia. Launch Vehicles: RT-2. Propellants: Solid. Stages: 15D24. Agency: TsKB-7.

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