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Isayev R-17
Status: Out of production. Date: 1958-64. Number: 15 . Thrust: 131.20 kN (29,495 lbf). Unfuelled mass: 120 kg (260 lb). Height: 1.49 m (4.88 ft). Diameter: 0.77 m (2.52 ft).
Thrust (sl): 131.210 kN (29,497 lbf). Thrust (sl): 13,380 kgf. Engine: 120 kg (260 lb). Propellant Formulation: AK27I/TM185. Thrust to Weight Ratio: 111.49.
Family: Storable liquid. Country: Russia. Launch Vehicles: R-17. Propellants: Nitric acid/Kerosene. Stages: R-17 stage. Agency: Isayev bureau. Bibliography: 342, 344.
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