Dersin Bilgileri

Dersin Adı	Türkçe	Rocket Propulsion
	İngilizce	Rocket Propulsion
Dersin Kodu	UZB 441E	Kredi	Ders (saat/hafta)	Uygulama (saat/hafta)	Labratuvar (saat/hafta)
Dönem	7	3	3	-	-
Dersin Dili		İngilizce
Dersin Koordinatörü		Kemal Bülent Yüceil
Dersin Amaçları		The objective is to give aerospace engineering students a firm understanding of rocket propulsion, the assumptions behind it, and the resulting limitations and applications.
Dersin Tanımı		CONTENT: Classification, Definition and Fundamentals, Nozzle Theory and Thermodynamic Relations, Flight Performance, Chemical Rocket Propellant Performance Analysis, Liquid Propellant Rocket Engine Fundamentals, Solid Propellant Rocket Fundamentals, Electric Propulsion
Dersin Çıktıları		Ability to understand the general aspects of theory and applications of rocket propulsion and to solve simple problems associated with the application of rocket propulsion. Gain an understanding of the application of rocket propulsion to spacecraft design and development in terms of choosing the proper rocket engine geometry and parameters for required design goals and investigating the impact of different rocket engine parameters on vehicle performance.
Önkoşullar		UZB362E Compressible Aerodynamics
Gereken Olanaklar		Students should have had an introductory course dealing with the fundamentals of compressible flow such as thermodynamic concepts, isentropic flow in a variable-area duct, Prandtl-Meyer flow and shock waves.
Diğer		Worksheets or some programming may be needed when solving the chemical reactions in combustion process.
Ders Kitabı		Rocket Propulsion Elements, 7th edition, G. P. Sutton, O. Biblarz, Wiley-Interscience, 2001.
Diğer Referanslar		Mechanics and Thermodynamics of Propulsion, Second Edition P.G. Hill & C.R. Peterson, Addison-Wesley, 1992 Aerothermodynamics of Gas Turbine and Rocket Propulsion, Third Edition, G. C. Oates, AIAA Education Series, 1997. Spacecraft Propulsion, Brown, C.D., AIAA Education Series, 1996 Modern Engineering for Design of Liquid-Propellant Rocket Engines, Huzel, D. K, D.H. Huang, AIAA Progress in Astronautics & Aeronautics, 1992.

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