OKB-1 solid rocket engine. 500 kN.
Gross mass: 10,000 kg (22,000 lb).
Unfuelled mass: 1,500 kg (3,300 lb).
Height: 4.00 m (13.10 ft).
Diameter: 1.49 m (4.88 ft).
Thrust: 500.00 kN (112,400 lbf).
Burn time: 30 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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RT-1-2 Solid rocket stage. 500.00 kN (112,404 lbf) thrust. Mass 10,000 kg (22,046 lb). More...
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