SNECMA solid rocket engine. 10.5 kN.
Gross mass: 50 kg (110 lb).
Unfuelled mass: 20 kg (44 lb).
Height: 2.10 m (6.80 ft).
Diameter: 0.13 m (0.42 ft).
Thrust: 10.50 kN (2,360 lbf).
Burn time: 5.30 s.
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Associated Countries
See also
Associated Manufacturers and Agencies
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SNECMA French manufacturer of rocket engines and rockets. SNECMA, France. More...
Associated Propellants
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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...
Associated Stages
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Aurore-1 Solid rocket stage. 10.50 kN (2,360 lbf) thrust. Mass 50 kg (110 lb). More...
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