Solid rocket stage. 900.00 kN (202,328 lbf) thrust. Mass 30,000 kg (66,139 lb).
Status: Active.
Gross mass: 30,000 kg (66,000 lb).
Unfuelled mass: 2,500 kg (5,500 lb).
Height: 6.50 m (21.30 ft).
Diameter: 2.30 m (7.50 ft).
Thrust: 900.00 kN (202,320 lbf).
Burn time: 60 s.
Number: 2 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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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