Encyclopedia Astronautica
M-100-100


Russian solid rocket engine.

Gross mass: 100 kg (220 lb).
Unfuelled mass: 55 kg (121 lb).
Height: 1.60 m (5.20 ft).
Diameter: 0.25 m (0.82 ft).
Burn time: 4.50 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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