Encyclopedia Astronautica
Chick


RO solid rocket engine. 60 kN.

Unfuelled mass: 6.00 kg (13.20 lb).
Height: 0.60 m (1.96 ft).
Diameter: 0.10 m (0.32 ft).
Thrust: 60.00 kN (13,488 lbf).
Burn time: 0.20 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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