Encyclopedia Astronautica
Mk7


Multiple-source solid rocket engine. 9.8 kN.

Gross mass: 10 kg (22 lb).
Unfuelled mass: 9.00 kg (19.80 lb).
Height: 1.20 m (3.90 ft).
Diameter: 0.0700 m (0.2290 ft).
Thrust: 9.80 kN (2,203 lbf).
Burn time: 0.90 s.

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Associated Countries
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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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