SEP solid rocket engine. 440 kN.
Gross mass: 10,000 kg (22,000 lb).
Height: 4.70 m (15.40 ft).
Diameter: 1.51 m (4.95 ft).
Thrust: 440.00 kN (98,910 lbf).
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Associated Countries
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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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SSBS S01-2 Solid propellant rocket stage. Loaded mass 10,000 kg. Thrust 440.00 kN. More...
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