Encyclopedia Astronautica
Topol'-M-1


Solid rocket stage. 980.00 kN (220,313 lbf) thrust. Mass 26,000 kg (57,320 lb).

AKA: Topol'-M1.
Status: Active.
Gross mass: 26,000 kg (57,000 lb).
Unfuelled mass: 3,000 kg (6,600 lb).
Height: 8.50 m (27.80 ft).
Diameter: 1.80 m (5.90 ft).
Thrust: 980.00 kN (220,310 lbf).
Burn time: 60 s.
Number: 19 .

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • 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...
  • Bulava Russian intercontinental ballistic missile. Solid-propellant Soviet intercontinental-range ballistic missile, equipped with multiple independently targeted warheads. 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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