NASDA solid rocket engine. 61 kN.
Total Impulse: -2 kNs.
Gross mass: 700 kg (1,540 lb).
Unfuelled mass: 200 kg (440 lb).
Height: 3.00 m (9.80 ft).
Diameter: 0.50 m (1.64 ft).
Thrust: 61.00 kN (13,713 lbf).
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Associated Countries
See also
Associated Manufacturers and Agencies
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NASDA Japanese agency overseeing development of rockets, spacecraft, and rocket engines. National Space Development Agency, Japan. More...
Associated Propellants
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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
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TT-500-2 Solid rocket stage. 61.00 kN (13,713 lbf) thrust. Mass 700 kg (1,543 lb). More...
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