Encyclopedia Astronautica
NAL-735


NASDA solid rocket engine. 250 kN.

Gross mass: 4,700 kg (10,300 lb).
Height: 9.00 m (29.50 ft).
Diameter: 0.74 m (2.42 ft).
Thrust: 250.00 kN (56,200 lbf).
Burn time: 49 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • NASDA Japanese agency overseeing development of rockets, spacecraft, and rocket engines. National Space Development Agency, 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
  • NAL-735-1 Solid propellant rocket stage. Loaded mass 4,700 kg. Thrust 250.00 kN. More...

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