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MIHT-1
Part of 15Zh58A Family
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.

AKA: Start-1. Status: In production. Number: 7 . Thrust: 980.60 kN (220,448 lbf). Gross mass: 26,000 kg (57,000 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 60 s. Height: 8.50 m (27.80 ft). Diameter: 1.61 m (5.28 ft).

Thrust (sl): 887.400 kN (199,495 lbf). Thrust (sl): 90,494 kgf.



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

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