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MIHT-4
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Application: Start-4. Gross Mass: 1,000 kg (2,200 lb). Empty Mass: 300 kg (660 lb). Propellants: Solid. Thrust(vac): 9.800 kN (2,203 lbf). Isp: 295 sec. Burn time: 207 sec. Diameter: 1.40 m (4.50 ft). Length: 2.50 m (8.20 ft). Chambers: 1. Country: Russia. Status: In production. First Flight: 1993. Last Flight: 2006. Flown: 7.00. Used in Start-4. Estimated values.
MIHT-4 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 Superseded by the later editions.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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© Mark Wade, 1997 - 2007 except where otherwise noted.
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