Buch, Englisch, Band 4, 850 Seiten, Format (B × H): 160 mm x 241 mm, Gewicht: 1449 g
Reihe: Space Technology Library
From Concept to Launch
Buch, Englisch, Band 4, 850 Seiten, Format (B × H): 160 mm x 241 mm, Gewicht: 1449 g
Reihe: Space Technology Library
ISBN: 978-0-7923-3476-7
Verlag: Springer Netherlands
For system engineers, mechanical designers, stress analysts, dynamics and load analysts, technical leads, program managers.
Zielgruppe
Research
Fachgebiete
- Mathematik | Informatik EDV | Informatik Angewandte Informatik Computeranwendungen in Wissenschaft & Technologie
- Technische Wissenschaften Technik Allgemein Computeranwendungen in der Technik
- Wirtschaftswissenschaften Wirtschaftssektoren & Branchen Fertigungsindustrie Luftfahrtindustrie
- Technische Wissenschaften Maschinenbau | Werkstoffkunde Technische Mechanik | Werkstoffkunde Statik, Dynamik, Kinetik, Kinematik
- Mathematik | Informatik EDV | Informatik Professionelle Anwendung Computer-Aided Design (CAD)
- Technische Wissenschaften Sonstige Technologien | Angewandte Technik Astronautik
- Technische Wissenschaften Verkehrstechnik | Transportgewerbe Fahrzeugtechnik
- Technische Wissenschaften Technik Allgemein Mathematik für Ingenieure
- Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr
Weitere Infos & Material
Preface. Part I: Introduction. 1. Developing Spacecraft Structures and Mechanisms. Part II: Requirements. 2. Developing Mechanical Requirements and Conceptual Designs. 3. Space Mission Environments. Part III: Analysis. 4. Structural Mechanics. 5. Loads Analysis for Single-Degree-of-Freedom Systems. 6. Mechanics of Materials. 7. Flexible-Body Dynamics. 8. Strength Analysis. 9. Structural Life Analysis. 10. Thermal Effects. Part IV: Verification and Quality Assurance. 11. Developing Confidence in Mechanical Designs and Products. 12. Verification Criteria. 13. Ensuring Quality. Part V: Design. 14. Configuring a Spacecraft. 15. Conceptual Design of Structures. 16. Idealizing and Modeling Structures. 17. Controlling Structural Responses. 18. Design Loads Cycles. 19. Developing Mechanisms. Part VI: Final Verification. 20. Designing for Producibility. 21. Final Verification. Appendixes: A. Units and Conversion Factors. B. Effective Verification Documentation. C. Structural Reliability Analysis. D. Standard Normal Probability Table. E. Preparing for and Documenting Tests. F. Spacecraft Integration and Test. G. Estimating Structural Damping. Index.