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15D24P

Engine · Russia

Original archive entry. The text, images and links below are kept as they were written.

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.

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