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astronautix.com 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.
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Last update 12 March 2001.
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