Engine Model: 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): 58.800 kN (13,219 lbf). Throttled thrust(vac): 5.900 kN (1,326 lbf). Isp (sea level): 230 sec. Burn time: 360 sec. Mass Engine: 86 kg (189 lb). Diameter: 0.30 m (0.98 ft). Length: 0.40 m (1.31 ft). Chambers: 2. Chamber Pressure: 66.00 bar. Thrust to Weight Ratio: 69.72. Country: Russia. Status: Out of Production. First Flight: 1960. 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.
Bibliography:- Burya article, Lavochkin web site.
- Haeseler, Dietrich, Visit to the museum of Chemical Automatics Design Bureau, Voronezh 1992 via Dietrich Haeseler.
- Russian Arms Catalogue, Vol 5 and 6, Military Parade, Moscow via Dietrich Haeseler.