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astronautix.com RD-2


Manufacturer Name: RD-2. Designer: Glushko. Developed in: 1945-47. Application: experimental. Propellants: Nitric acid/Kerosene Thrust(vac): 612 kgf. Thrust(vac): 6.00 kN. Isp: 200 sec. Mass Engine: 71 kg. Chambers: 1. Chamber Pressure: 20.60 bar. Country: Russia. Status: Developed 1945-47. References: 342 . Comments: The RD-2 was based on the RD-1 engine. Used chemical ignition.
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Last update 12 March 2001.
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