Rocket Propulsion

Autorentext
Stephen Heister is the Raisbeck Distinguished Professor of Aeronautical Engineering at Purdue University, Indiana, and has previously worked in industry. He has served as an Associate Editor of The AIAA Journal of Propulsion and Power and is an elected Fellow of the American Institute of Aeronautics and Astronautics (AIAA).

Klappentext
Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.

Zusammenfassung
Equips students with a thorough up-to-date knowledge of rocket propulsion, along with practical tools that can be applied in industry. Numerous homework problems, an online solutions manual, real-life case studies and examples, numerical methods, and links to online materials are all included. Ideal for senior and first year graduate students.

Inhalt
1. Classification of rocket propulsion systems and historical perspective; 2. Mission analysis fundamentals; 3. Trajectory analysis and rocket design; 4. Ideal rocket nozzle performance; 5. Combustion and thermochemistry; 6. Heat transfer; 7. Solid rocket motors (SRMs); 8. Liquid rocket engines (LREs); 9. Liquid rocket propellants; 10. Turbomachinery fundamentals; 11. Hybrid rocket engines (HREs); 12. Combustion instability; 13. Electric propulsion fundamentals.

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