ISAS solid rocket engine. 105 kN.
Height: 3.30 m (10.80 ft).
Diameter: 0.33 m (1.08 ft).
Thrust: 105.00 kN (23,604 lbf).
Burn time: 3.00 s.
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Associated Countries
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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...
Associated Stages
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