This page no longer updated from 31 October 2001. Latest version can be found at Glushko C

Designer: Glushko. Thrust(vac): 3,000,000 kgf. Chambers: 1. Country: USSR. Status: Study 1970. References: 283 . Comments: Glushko studied liquid propellant engines of 'several thousand tonnes thrust' in the period 1963-1970. Largest thrust chamber ever tested in Russia was Glushko's RD-270 of 680 tf.
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Last update 12 March 2001.
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© Mark Wade, 2001 .