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MIHT-1
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Application: Start-1. Gross Mass: 26,000 kg (57,000 lb). Empty Mass: 3,000 kg (6,600 lb). Propellants: Solid. Thrust(vac): 980.600 kN (220,448 lbf). Thrust(sl): 887.400 kN (199,495 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 60 sec. Diameter: 1.61 m (5.28 ft). Length: 8.50 m (27.80 ft). Chambers: 1. Country: Russia. Status: In production. First Flight: 1993. Last Flight: 2006. Flown: 7.00. Used in Start-1. Estimated values.
MIHT-1 used on Rocket Stages
Bibliography and Further Reading - Isakowitz, Steven J,, International Reference to Space Launch Systems Second Edition, AIAA, Washington DC, 1991 (succeeded by 2000 edition). ISBN: 1563473534. Superseded by the later editions. More at amazon.com...
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