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MIHT-3
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Application: Start-3. Gross Mass: 6,000 kg (13,200 lb). Empty Mass: 1,000 kg (2,200 lb). Propellants: Solid. Thrust(vac): 245.200 kN (55,123 lbf). Thrust(sl): 192.600 kN (43,298 lbf). Isp: 280 sec. Isp (sea level): 220 sec. Burn time: 56 sec. Diameter: 1.50 m (4.90 ft). Length: 3.00 m (9.80 ft). Chambers: 1. Country: Russia. Status: In production. First Flight: 1993. Last Flight: 2006. Flown: 7.00. Used in Start-3. Estimated values.
MIHT-3 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 Superseded by the later editions.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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