Encyclopedia Astronautica
TR-1-7500


NASDA solid rocket engine. 608 kN.

Gross mass: 7,500 kg (16,500 lb).
Unfuelled mass: 4,000 kg (8,800 lb).
Height: 7.00 m (22.90 ft).
Diameter: 1.10 m (3.60 ft).
Thrust: 608.00 kN (136,683 lbf).
Burn time: 52 s.

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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...

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