15D24
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
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.