This page no longer updated from 31 October 2001. Latest version can be found at RD-102

Manufacturer Name: RD-102. Other Designations: RD-3A. Designer: Glushko. Application: R-3A. Used on stages: R-3A. Used on launch vehicles: R-3A. Propellants: Lox/Alcohol Thrust(vac): 43,700 kgf. Thrust(vac): 428.00 kN. Isp: 235 sec. Isp (sea level): 214 sec. Burn time: 83 sec. Chambers: 1. Country: Russia. Status: Developed 1950's. References: 283 . Comments: Project for R-3A experimental missile. Stopped in favor of RD-103.
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Last update 12 March 2001.
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© Mark Wade, 2001 .