Encyclopedia Astronautica
SB-310


ISAS solid rocket engine. 95 kN.

Gross mass: 500 kg (1,100 lb).
Unfuelled mass: 190 kg (410 lb).
Height: 5.80 m (19.00 ft).
Diameter: 0.31 m (1.01 ft).
Thrust: 95.00 kN (21,356 lbf).
Burn time: 7.40 s.

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Associated Countries
See also
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...

Associated Stages
  • Mu-3C-0 Solid rocket stage. 95.00 kN (21,357 lbf) thrust. Mass 500 kg (1,102 lb). More...

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