Thiokol solid rocket engine. 45 kN. Out of Production. Total impulse 190,590 kgf-sec. Motor propellant mass fraction 0.925. Isp=287s.
Status: Out of Production.
Gross mass: 711 kg (1,567 lb).
Unfuelled mass: 53 kg (116 lb).
Diameter: 0.93 m (3.07 ft).
Thrust: 45.00 kN (10,116 lbf).
Specific impulse: 287 s.
Number: 20 .
More... - Chronology...
Associated Countries
See also
Associated Manufacturers and Agencies
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Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, USA. 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...
Bibliography
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Thiokol Corporation Web Site, As of May, 1999. Web Address when accessed: here.
Associated Stages
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Star 37S Solid rocket stage. 45.00 kN (10,116 lbf) thrust. Mass 711 kg (1,567 lb). More...
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