Thiokol solid rocket engine. 55.5 kN. Out of Production. Total impulse 249,177 kgf-sec. Motor propellant mass fraction 0.928. Isp=286s.
Status: Out of Production.
Gross mass: 934 kg (2,059 lb).
Unfuelled mass: 67 kg (147 lb).
Diameter: 0.93 m (3.07 ft).
Thrust: 55.50 kN (12,477 lbf).
Specific impulse: 286 s.
Burn time: 42 s.
Number: 19 .
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 37F Solid rocket stage. 55.50 kN (12,477 lbf) thrust. Mass 934 kg (2,059 lb). More...
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