This page no longer updated from 31 October 2001. Latest version can be found at RD-3A

Manufacturer Name: RD-3A. Other Designations: RD-102?. Designer: Glushko. Developed in: 1951-53. Application: R-3A. Propellants: Lox/Alcohol Isp (sea level): 214 sec. Mass Engine: 885 kg. Length: 3.1 m. Chambers: 1. Oxidizer to Fuel Ratio: 0.00. Country: Russia. Status: Out of Production. References: 21 , 283 . Comments: Project for R-3A experimental missile. Stopped in favour of RD-103.
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Last update 12 March 2001.
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© Mark Wade, 2001 .