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RD-302
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Manufacturer Name: RD-302. Government Designation: 11D130F. Other Designations: 11D130F. Designer: Glushko. Developed in: 1960-69. Propellants: LF2/Ammonia. Thrust(vac): 98.000 kN (22,031 lbf). Isp: 405 sec. Chambers: 1. Chamber Pressure: 117.60 bar. Country: Russia. Status: Developed 1960-69. Successor to RD-303 and predecessor to RD-301. Staged combustion cycle. Bibliography and Further Reading - Rakhmanin, V F, Odnazhdy i Navsegda, NPO Energomash, Moscow 1998 via Dietrich Haeseler. Biography and history of development of the rocket motors of Glushko.
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