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E-raamat: Introduction to Spacecraft Thermal Design

(University of Maryland, College Park)
  • Formaat: EPUB+DRM
  • Sari: Cambridge Aerospace Series
  • Ilmumisaeg: 09-Jul-2020
  • Kirjastus: Cambridge University Press
  • Keel: eng
  • ISBN-13: 9781108152037
  • Formaat - EPUB+DRM
  • Hind: 123,49 €*
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  • Formaat: EPUB+DRM
  • Sari: Cambridge Aerospace Series
  • Ilmumisaeg: 09-Jul-2020
  • Kirjastus: Cambridge University Press
  • Keel: eng
  • ISBN-13: 9781108152037

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"Develop a fundamental understanding of heat transfer analysis techniques as applied to earth based spacecraft with this practical guide. Written in a tutorial style, this essential text provides a how-to manual tailored for those who wish to understand and develop spacecraft thermal analyses. Providing an overview of basic heat transfer analysis fundamentals such as thermal circuits, limiting resistance, MLI, environmental thermal sources and sinks, as well as contemporary space based thermal technologies, and the distinctions between design considerations inherent to room temperature and cryogenic temperature applications, this is the perfect tool for graduate students, professionals and academic researchers"--

Arvustused

'The text provides a comprehensive overview of the thermophysical processes, operating principles, governing equations and solution methods for spacecraft thermal design. Unlike over standard heat transfer textbooks, the system design issues are presented and analyzed in detail with respect to a space environment that considers both earth-based and deep-space missions. Another strength of the book is its diverse set of worked examples throughout each chapter and end-of-chapter problems. This book serves as an excellent learning resource for students and valuable reference for all professionals and researchers who are working on spacecraft design.' Greg F. Naterer, Memorial University of Newfoundland 'Introduction to Spacecraft Thermal Design thoroughly fills a much needed gap in a growing field. Bringing together the fundamentals of heat transfer, the uniqueness of the space environment and the essentials of thermal design, it is a useful text and handy guide for student and experienced practitioner alike.' Mike Pauken, Jet Propulsion Laboratory, California Institute of Technology

Muu info

Develop a fundamental understanding of heat transfer analysis techniques as applied to earth based spacecraft with this practical guide.
List of Figures
xi
List of Tables
xix
Nomenclature xxi
Subscripts xxvi
1 Introduction
1(12)
1.1 Background
1(1)
1.2 Why Is Space Important?
1(2)
1.3 Space-Based Thermal Energy Analysis Constructs
3(1)
1.4 Units
4(1)
1.5 Fundamental Heat Transfer Mechanisms
5(4)
1.6 The Energy Balance
9(1)
1.7 Supplemental Resources
10(3)
2 Conduction Heat Transfer Analysis
13(51)
2.1 Introduction
13(1)
2.2 1-D Conduction
13(12)
2.3 Finite Difference, Finite Element and the Energy Balance
25(12)
2.4 Radial Geometries
37(5)
2.5 2-D Conduction Shape Factors
42(2)
2.6 Honeycomb Panel Structures
44(2)
2.7 Lumped Body Heating Methodology
46(18)
3 Radiative Heat Transfer Analysis
64(50)
3.1 Fundamentals of Radiation
64(1)
3.2 The Blackbody
65(6)
3.3 Real Surfaces
71(6)
3.4 Radiative Heat Transfer between Surfaces
77(19)
3.5 Multilayer Insulation
96(18)
4 The Space Environment
114(51)
4.1 Design Considerations
114(2)
4.2 Earth-Based vs. Deep Space Missions
116(3)
4.3 Astrodynamics Fundamentals
119(2)
4.4 Lagrange Points
121(2)
4.5 Environmental Thermal Heating
123(8)
4.6 Analysis Methodologies
131(8)
4.7 Reduced Node SpaceCube Analysis
139(26)
5 Space-Based Advanced Thermal Conductance and Storage Technologies
165(98)
5.1 Space-Based Technologies
165(1)
5.2 Transfer Processes
165(2)
5.3 Fundamental Technologies
167(14)
5.4 Boiling Heat Transfer Components in 1-g and Microgravity
181(35)
5.5 Thermoelectric Coolers and Generators
216(10)
5.6 Phase Change Materials
226(37)
6 Sensors, Instrumentation and Test Support Hardware
263(21)
6.1 Introduction
263(1)
6.2 What Is a Sensor?
263(5)
6.3 Heaters
268(4)
6.4 Test Support Equipment
272(4)
6.5 Error Analysis
276(8)
7 Fundamentals of Cryogenics
284(49)
7.1 Background
284(1)
7.2 Materials at Cryogenic Temperatures
285(8)
7.3 Transfer Processes at Low Temperature
293(7)
7.4 Design Features of Cryogenic Systems
300(3)
7.5 Standard Methods for Cool-Down
303(30)
8 Developmental and Environmental Testing
333(8)
8.1 Background
333(1)
8.2 Spacecraft Systems Test Philosophy
334(3)
8.3 Assembly-Level Testing
337(1)
8.4 Cryogenic Considerations
338(3)
Appendix A 341(4)
Appendix B 345(7)
Appendix C 352(3)
Index 355(6)
Solutions 361
Eric A. Silk is a lecturer in the Aerospace Engineering Department at the University of Maryland with twenty-two years of engineering experience in spacecraft/instrument thermal modelling, applied thermodynamics, high heat flux cooling systems, and thermal control system design and analysis.