This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Kartukov. Developed in: 1956-. Application: DBR-1 Yastreb. Propellants: Solid Thrust(vac): 80,000 kgf. Thrust(vac): 784.00 kN. Country: Russia. Status: Out of Production. Comments: Thrust 80 tf at ignition, 75 tf at cutout.
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Last update 12 March 2001.
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© Mark Wade, 2001 .