MIHT-1
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
MIHT solid rocket engine. Start-1. In production. Used in Start-1. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated. Start first stage.
Thrust (sl): 887.400 kN (199,495 lbf). Thrust (sl): 90,494 kgf.