Solid rocket stage. 44.50 kN (10,004 lbf) thrust. Mass 1,000 kg (2,205 lb).
Status: Retired 1978.
Gross mass: 1,000 kg (2,200 lb).
Unfuelled mass: 240 kg (520 lb).
Height: 5.10 m (16.70 ft).
Diameter: 0.44 m (1.44 ft).
Thrust: 44.50 kN (10,004 lbf).
Burn time: 30 s.
Number: 21 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Skylark 1 British sounding rocket. Two stage Skylark version consisting of 1 x Raven 8 + 1 x Raven 1/1A/2A More...
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...
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