Encyclopedia Astronautica
Star 37XF



star37xf.jpg
Star-37XF
Credit: Thiokol
Thiokol solid rocket engine. 45 kN. Out of Production. Total flown included in total for Star-37XF-8. Total impulse 259,123 kgf-sec. Motor propellant mass fraction 0.929. Isp=290s.

Status: Out of Production.
Gross mass: 953 kg (2,101 lb).
Unfuelled mass: 68 kg (149 lb).
Diameter: 0.93 m (3.06 ft).
Thrust: 45.00 kN (10,116 lbf).
Specific impulse: 290 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, USA. 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...

Bibliography
  • Thiokol Corporation Web Site, As of May, 1999. Web Address when accessed: here.

Associated Stages
  • Star 37XF Solid rocket stage. 45.00 kN (10,116 lbf) thrust. Mass 953 kg (2,101 lb). More...

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