Encyclopedia Astronautica
K150


ISAS solid rocket engine. 19 kN.

Gross mass: 100 kg (220 lb).
Unfuelled mass: 10 kg (22 lb).
Height: 3.50 m (11.40 ft).
Diameter: 0.15 m (0.49 ft).
Thrust: 19.00 kN (4,271 lbf).
Burn time: 16 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
  • Kappa 6H-2 Solid rocket stage. 19.00 kN (4,271 lbf) thrust. Mass 100 kg (220 lb). More...

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