Encyclopedia Astronautica
M-100-300


Russian solid rocket engine.

Gross mass: 300 kg (660 lb).
Unfuelled mass: 110 kg (240 lb).
Height: 3.50 m (11.40 ft).
Diameter: 0.25 m (0.82 ft).
Burn time: 5.00 s.

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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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