Solid propellant rocket stage. Loaded mass 1,500 kg. Thrust 200.00 kN.
Status: Retired 1961.
Gross mass: 1,500 kg (3,300 lb).
Height: 2.50 m (8.20 ft).
Diameter: 0.56 m (1.83 ft).
Thrust: 200.00 kN (44,960 lbf).
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Associated Countries
Associated Engines
Associated Launch Vehicles
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SE.4400 French surface-to-air missile. SNCASE missile design using a Stromboli booster and two ramjet sustainers. More...
Associated Manufacturers and Agencies
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Sud French manufacturer of rocket engines. Sud Aviation, 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...
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