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Engine Model: RD-3A. Manufacturer Name: RD-3A. Other Designations: RD-102?. Designer: Glushko. Developed in: 1951-53. Application: R-3A. Propellants: Lox/Alcohol. Thrust(sl): 390.000 kN (87,670 lbf). Isp (sea level): 214 sec. Mass Engine: 885 kg (1,951 lb). Length: 3.12 m (10.24 ft). Chambers: 1. Oxidizer to Fuel Ratio: 0.00. Country: Russia. Status: Out of Production. Project for R-3A experimental missile. Stopped in favour of RD-103.
Bibliography:- Semenov, Yuri P Editor, Raketno-kosmicheskaya korporatsiya 'Energia' imeni S P Koroleva, Moscow, Russia, 1996.
- Vetrov, G S, S. P. Korolev i evo delo, Nauka, Moscow, 1998.
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