15D23
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
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.