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astronautix.com RD-0201


Manufacturer Name: RD-0201. Designer: Kosberg. Developed in: 1957-60. Application: SAM V1100 by Grushin stage 3. Propellants: Nitric acid/Amine Thrust(vac): 5,920 kgf. Thrust(vac): 58.06 kN. Isp: 260 sec. Burn time: 180 sec. Mass Engine: 120 kg. Diameter: 0.4 m. Length: 0.7 m. Chambers: 4. Chamber Pressure: 62.00 bar. Country: Russia. Status: Out of Production. First Flight: 1960. References: 307 , 342 . Comments: Thrust range 59 - 28 kN.
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Last update 12 March 2001.
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