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University of Tennessee, Knoxville    
  Jan 23, 2018
2015-2016 Graduate Catalog [ARCHIVED CATALOG]

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AE 581 - Rocket Propulsion I

3 Credit Hours
Rocket propulsion fundamentals; thermodynamics of nonreacting and chemically reacting ideal gases, rocket nozzle design; ideal rocket performance parameters; rocket heat transfer; chemistry of propellants; liquid rocket engine systems; ground testing; introduction to solid propellant rockets.
Registration Permission: Consent of Instructor.

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