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Engine Model: 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): 58.060 kN (13,052 lbf). Throttled thrust(vac): 28.000 kN (6,294 lbf). Isp: 260 sec. Burn time: 180 sec. Mass Engine: 120 kg (260 lb). Diameter: 0.40 m (1.31 ft). Length: 0.70 m (2.29 ft). Chambers: 4. Chamber Pressure: 62.00 bar. Thrust to Weight Ratio: 49.33. Country: Russia. Status: Out of Production. First Flight: 1960. Thrust range 59 - 28 kN.
Bibliography:- 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.
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