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MIHT-4
MIHT solid rocket engine. Start-4. In production. Used in Start-4. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated.

AKA: 15Zh58D. Status: In production. Number: 7 . Thrust: 9.80 kN (2,203 lbf). Gross mass: 1,000 kg (2,200 lb). Unfuelled mass: 300 kg (660 lb). Specific impulse: 295 s. Burn time: 207 s. Height: 2.50 m (8.20 ft). Diameter: 1.40 m (4.50 ft).



People: Nadiradze. Country: Russia. Launch Vehicles: Start-1, Start, Start-1.2. Propellants: Solid. Stages: MIHT-4. Bibliography: 42.

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