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UPAero solid rocket engine. 45 kN.

Gross mass: 200 kg (440 lb).
Height: 4.00 m (13.10 ft).
Diameter: 0.27 m (0.88 ft).
Thrust: 45.00 kN (10,116 lbf).
Burn time: 14 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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