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MIHT-2
Part of 15Zh58B Family
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.

AKA: Start-2. Status: In production. Number: 8 . Thrust: 490.30 kN (110,224 lbf). Gross mass: 13,000 kg (28,000 lb). Unfuelled mass: 1,500 kg (3,300 lb). Specific impulse: 280 s. Specific impulse sea level: 220 s. Burn time: 64 s. Height: 6.00 m (19.60 ft). Diameter: 1.55 m (5.08 ft).

Thrust (sl): 385.300 kN (86,619 lbf). Thrust (sl): 39,286 kgf.



People: Nadiradze. Country: Russia. Launch Vehicles: Topol', Start-1, Start, Start-1.2. Propellants: Solid. Stages: MIHT-2. Bibliography: 42.

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