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Engine Model: Isayev R-17. Designer: Isayev. Developed in: 1958-64. Application: R-17. Propellants: Nitric acid/Kerosene. Thrust(vac): 131.200 kN (29,495 lbf). Thrust(sl): 131.210 kN (29,497 lbf). Mass Engine: 120 kg (260 lb). Diameter: 0.77 m (2.52 ft). Length: 1.49 m (4.88 ft). Chambers: 1. Thrust to Weight Ratio: 111.49. Country: Russia. Status: Out of production. First Flight: 1961. Last Flight: 2004. Flown: 15. Designation unknown.
Isayev R-17 used on Rocket Stages - Used on stage: R-17. on launch vehicle: R-17.
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