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.

Bibliography and Further Reading
  • Russian Arms Catalogue, Vol 5 and 6, Military Parade, Moscow via Dietrich Haeseler.
 
 
 
 
 
 
 
 
 

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