MITT solid rocket engine. 490 kN.
Gross mass: 13,000 kg (28,000 lb).
Unfuelled mass: 1,500 kg (3,300 lb).
Height: 6.00 m (19.60 ft).
Diameter: 1.55 m (5.08 ft).
Thrust: 490.00 kN (110,150 lbf).
Burn time: 64 s.
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Associated Countries
See also
Associated Manufacturers and Agencies
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Nadiradze Russian manufacturer of rocket engines and rockets. Nadiradze, Russia. 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...
Associated Stages
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Topol'-M-2 Solid rocket stage. 490.00 kN (110,156 lbf) thrust. Mass 13,000 kg (28,660 lb). More...
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