MIHT-2
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
solid rocket engine. Start-2. In production. Used in Start-2. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated except stage gross mass. Start second stage.
Thrust (sl): 385.300 kN (86,619 lbf). Thrust (sl): 39,286 kgf.