Solid propellant rocket stage. Loaded mass 100 kg.
Status: Retired 1965.
Gross mass: 100 kg (220 lb).
Height: 0.50 m (1.64 ft).
Diameter: 0.30 m (0.98 ft).
Number: 1 .
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Associated Countries
Associated Engines
Associated Launch Vehicles
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Kappa 10S Japanese sounding rocket. Three stage vehicle consisting of 1 x K420H + 1 x K420(1/3) + 1 x K10S More...
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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