This page no longer updated from 31 October 2001. Latest version can be found at 8D725

Government Designation: 8D725. Designer: Glushko. Developed in: 1963-1970. Propellants: N2O4/UDMH Thrust(vac): 12,000 kgf. Thrust(vac): 117.00 kN. Isp: 325 sec. Chambers: 1. Country: Russia. Status: Developed 1963-1970. References: 283 . Comments: 10 to 12 tonne thrust engine developed for an unstated military requirement.
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Last update 12 March 2001.
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