This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
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.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .