RO solid rocket engine. 105 kN.
Gross mass: 1,300 kg (2,800 lb).
Unfuelled mass: 290 kg (630 lb).
Height: 5.50 m (18.00 ft).
Diameter: 0.44 m (1.44 ft).
Thrust: 105.00 kN (23,604 lbf).
Burn time: 39 s.
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Associated Countries
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Associated Manufacturers and Agencies
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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Skylark 12-2 Solid rocket stage. 105.00 kN (23,605 lbf) thrust. Mass 1,300 kg (2,866 lb). More...
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