Matra solid rocket engine. 14.8 kN.
Gross mass: 20 kg (44 lb).
Unfuelled mass: 13 kg (28 lb).
Height: 0.80 m (2.62 ft).
Diameter: 0.13 m (0.42 ft).
Thrust: 14.80 kN (3,327 lbf).
Burn time: 1.00 s.
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Associated Countries
See also
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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Emma-0 Solid rocket stage. 14.80 kN (3,327 lbf) thrust. Mass 20 kg (44 lb). More...
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