Encyclopedia Astronautica
L735


ISAS solid rocket engine. 410 kN.

Gross mass: 5,000 kg (11,000 lb).
Unfuelled mass: 2,945 kg (6,492 lb).
Height: 8.40 m (27.50 ft).
Diameter: 0.74 m (2.42 ft).
Thrust: 410.00 kN (92,170 lbf).
Burn time: 29 s.

More... - Chronology...


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
  • Lambda 3-1 Solid rocket stage. 410.00 kN (92,172 lbf) thrust. Mass 5,000 kg (11,023 lb). More...

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