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8D725
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Government Designation: 8D725. Designer: Glushko. Developed in: 1963-1970. Propellants: N2O4/UDMH. Thrust(vac): 117.000 kN (26,302 lbf). Isp: 325 sec. Chambers: 1. Country: Russia. Status: Developed 1963-1970. 10 to 12 tonne thrust engine developed for an unstated military requirement.
Bibliography and Further Reading - Vetrov, G S, S. P. Korolev i evo delo, Nauka, Moscow, 1998. ISBN: 5020036846. The collected papers of Soviet Chief Designer Korolev. A tremendous source of new information and insight on the Soviet space program. Russian language. More at amazon.com...
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