Encyclopedia Astronautica
Temp-2S-3


Solid rocket stage. 245.00 kN (55,078 lbf) thrust. Mass 8,700 kg (19,180 lb).

Status: Retired 1988.
Gross mass: 8,700 kg (19,100 lb).
Unfuelled mass: 1,000 kg (2,200 lb).
Height: 3.90 m (12.70 ft).
Diameter: 1.34 m (4.39 ft).
Thrust: 245.00 kN (55,078 lbf).

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • Temp-2S Russian intercontinental ballistic missile. World's first operational mobile ICBM. Deployed in greaty secrecy in 1976-1987 contrary to the terms of the SALT-2 Treaty. More...

Associated Manufacturers and Agencies
  • Nadiradze Russian manufacturer of rocket engines and rockets. Nadiradze, Russia. More...

Associated Propellants
  • Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

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