Solid rocket stage. 110.00 kN (24,729 lbf) thrust. Mass 1,400 kg (3,086 lb).
Status: Retired 1963.
Gross mass: 1,400 kg (3,000 lb).
Unfuelled mass: 300 kg (660 lb).
Height: 8.70 m (28.50 ft).
Diameter: 0.42 m (1.37 ft).
Thrust: 110.00 kN (24,720 lbf).
Burn time: 17 s.
Number: 2 .
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Associated Countries
Associated Launch Vehicles
Associated Manufacturers and Agencies
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ISAS Japanese agency overseeing development of rockets, spacecraft, and rocket engines. Institute of Space and Astronautical Science, Japan. More...
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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