Solid propellant rocket stage. Loaded mass 11,600 kg. Thrust 979.00 kN.
Status: Retired 1991.
Gross mass: 11,600 kg (25,500 lb).
Height: 7.50 m (24.60 ft).
Diameter: 1.17 m (3.83 ft).
Thrust: 979.00 kN (220,087 lbf).
Burn time: 40 s.
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Associated Countries
Associated Engines
Associated Launch Vehicles
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SICBM American mobile small intercontinental ballistic missile. Developed 1986-1991, but cancelled as unnecessary at the end of the Cold War. More...
Associated Manufacturers and Agencies
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Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, USA. More...
Associated Propellants
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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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