Solid rocket stage. 245.00 kN (55,078 lbf) thrust. Mass 6,000 kg (13,228 lb).
AKA: Topol'-M3.
Status: Active.
Gross mass: 6,000 kg (13,200 lb).
Unfuelled mass: 1,000 kg (2,200 lb).
Height: 3.10 m (10.10 ft).
Diameter: 1.34 m (4.39 ft).
Thrust: 245.00 kN (55,078 lbf).
Burn time: 56 s.
Number: 19 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Topol M All-Russian solid propellant ICBM set to replace all older models in the first decade of the 21st Century. Designed for mobile deployment on 8-axis transport-launcher RT-2M2/SS-X-29), or placement in existing UR-100N and R-36M silos (RT-2M1/SS-X-27). More...
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Bulava Russian intercontinental ballistic missile. Solid-propellant Soviet intercontinental-range ballistic missile, equipped with multiple independently targeted warheads. More...
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...
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