This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Application: Start-4. Used on stages: Start-4. Used on launch vehicles: Start, Start-1. Gross Mass: 1,000 kg. Empty Mass: 300 kg. Propellants: Solid Thrust(vac): 1,000 kgf. Thrust(vac): 9.80 kN. Isp: 295 sec. Burn time: 207 sec. Diameter: 1.4 m. Length: 2.5 m. Chambers: 1. Country: Russia. Status: In Production. First Flight: 1993. Last Flight: 1997. Flown: 4. References: 42 . Comments: Used in Start-4. Estimated values.
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Last update 12 March 2001.
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© Mark Wade, 2001 .