Encyclopedia Astronautica
L735(1/3)


ISAS solid rocket engine. 118 kN.

Gross mass: 2,500 kg (5,500 lb).
Height: 3.90 m (12.70 ft).
Diameter: 0.74 m (2.42 ft).
Thrust: 118.00 kN (26,527 lbf).
Burn time: 38 s.

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Associated Countries
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Associated Manufacturers and Agencies
  • ISAS Japanese agency overseeing development of rockets, spacecraft, and rocket engines. Institute of Space and Astronautical Science, Japan. More...

Associated Propellants
  • 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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