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MIHT-3
Part of 15Zh58V Family
MIHT solid rocket engine. Start-3. In production. Used in Start-3. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated.

Status: In production. Number: 7 . Thrust: 245.20 kN (55,123 lbf). Gross mass: 6,000 kg (13,200 lb). Unfuelled mass: 1,000 kg (2,200 lb). Specific impulse: 280 s. Specific impulse sea level: 220 s. Burn time: 56 s. Height: 3.00 m (9.80 ft). Diameter: 1.50 m (4.90 ft).

Thrust (sl): 192.600 kN (43,298 lbf). Thrust (sl): 19,643 kgf.



People: Nadiradze. Country: Russia. Launch Vehicles: Topol', Start-1, Start, Start-1.2. Propellants: Solid. Stages: MIHT-3. Bibliography: 42.

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