ISAS solid rocket engine. 7.8 kN.
Gross mass: 100 kg (220 lb).
Unfuelled mass: 15 kg (33 lb).
Height: 0.50 m (1.64 ft).
Diameter: 0.48 m (1.57 ft).
Thrust: 7.80 kN (1,754 lbf).
Burn time: 32 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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