MIHT-3
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
MIHT solid rocket engine. Start-3. In production. Used in Start-3. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated.
Thrust (sl): 192.600 kN (43,298 lbf). Thrust (sl): 19,643 kgf.