American solid rocket engine. 690 kN.
Gross mass: 2,500 kg (5,500 lb).
Height: 10.20 m (33.40 ft).
Diameter: 0.66 m (2.16 ft).
Thrust: 690.00 kN (155,110 lbf).
Burn time: 3.00 s.
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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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