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๐Ÿ“

Modern Engineering for Design of Liquid-Propellant Rocket Engines

โœ Scribed by Huzel, Dieter K.; Huang, David H.


Publisher
American Institute of Aeronautics and Astronautics
Year
1992
Tongue
English
Leaves
467
Category
Library

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โœฆ Synopsis


From the component design to the subsystem design to the engine systems design, engine development, and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry.
- Data and information appearing in this book are for informational purposes only. AIAA and the author are not responsible for any injury or damage resulting from use or reliance, nor do AIAA and the author warrant that use or reliance will be free from privately owned rights.

โœฆ Table of Contents



Content:
Front Matter
• Preface
• Table of Contents
1. Introduction to Liquid-Propellant Rocket Engines
2. Engine Requirements and Preliminary Design Analyses
3. Introduction to Sample Calculations
4. Design of Thrust Chambers and Other Combustion Devices
5. Design of Gas-Pressurized Propellant Feed Systems
6. Design of Turbopump Propellant Feed Systems
7. Design of Rocket-Engine Control and Condition-Monitoring Systems
8. Design of Propellant Tanks
9. Design of Interconnecting Components and Mounts
10. Engine Systems Design Integration
11. Design of Liquid-Propellant Space Engines
• Appendix A: Weight Considerations
• Appendix B: Reliability Considerations
• Appendix C: Rocket Engine Materials
• List of Illustrations
• List of Tables
• List of Acronyms
Index


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