Encyclopedia Astronautica
15Zh58A


MITT solid rocket engine. 980 kN.

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.

More... - Chronology...


Associated Countries
See also
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...

Associated Stages
  • Topol'-M-1 Solid rocket stage. 980.00 kN (220,313 lbf) thrust. Mass 26,000 kg (57,320 lb). More...

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