Book contents
- Introduction to Spacecraft Thermal Design
- Cambridge Aerospace Series
- Introduction to Spacecraft Thermal Design
- Copyright page
- Dedication
- Contents
- Figures
- Tables
- Nomenclature
- Subscripts
- 1 Introduction
- 2 Conduction Heat Transfer Analysis
- 3 Radiative Heat Transfer Analysis
- 4 The Space Environment
- 5 Space-Based Advanced Thermal Conductance and Storage Technologies
- 6 Sensors, Instrumentation and Test Support Hardware
- 7 Fundamentals of Cryogenics
- 8 Developmental and Environmental Testing
- Book part
- Index
- Solutions
- References
3 - Radiative Heat Transfer Analysis
Published online by Cambridge University Press: 19 June 2020
Book contents
- Introduction to Spacecraft Thermal Design
- Cambridge Aerospace Series
- Introduction to Spacecraft Thermal Design
- Copyright page
- Dedication
- Contents
- Figures
- Tables
- Nomenclature
- Subscripts
- 1 Introduction
- 2 Conduction Heat Transfer Analysis
- 3 Radiative Heat Transfer Analysis
- 4 The Space Environment
- 5 Space-Based Advanced Thermal Conductance and Storage Technologies
- 6 Sensors, Instrumentation and Test Support Hardware
- 7 Fundamentals of Cryogenics
- 8 Developmental and Environmental Testing
- Book part
- Index
- Solutions
- References
Summary
In Chapter 1 the Stefan‒Boltzmann Law (shown in equation 3.1) was presented as the relation used to determine the amount of radiative thermal energy emitted from a surface.
- Type
- Chapter
- Information
- Introduction to Spacecraft Thermal Design , pp. 64 - 113Publisher: Cambridge University PressPrint publication year: 2020
References
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Finckener, M.M., and Dooling, D., 1999, “Multilayer Insulation Material Guidelines,” NASA/TP-1999-209263, Marshall Space Flight Center and D2 AssociatesGoogle Scholar
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