This page no longer updated from 31 October 2001. Latest version can be found at RD-0200

Manufacturer Name: RD-0200. Other Designations: RO1-154. Designer: Kosberg. Developed in: 1957-62. Application: SAM by Lavochkin on stage 2. Propellants: Nitric acid/Amine Thrust(vac): 5,996 kgf. Thrust(vac): 58.80 kN. Isp (sea level): 230 sec. Burn time: 360 sec. Mass Engine: 86 kg. Diameter: 0.3 m. Length: 0.4 m. Chambers: 2. Chamber Pressure: 66.00 bar. Country: Russia. Status: Out of Production. First Flight: 1960. References: 95 , 307 , 342 . Comments: The first liquid rocket engine of OKB-154, engine was developed on a basis of the S2.1200 engine, developed by Isayev's OKB-2 of GKOT and transferred to OKB-154. Thrust range 59 - 5.9 kN. Sea level specific impulse 230 - 166 sec.
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 .