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
5 - Space-Based Advanced Thermal Conductance and Storage Technologies
Published online by Cambridge University Press: 19 June 2020
- 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
At the end of Chapter 4 we had begun to perform temperature analysis of components internal to a SpaceCube in LEO. In the analysis procedure we determined that it would be necessary to implement a thermal coupling between the E-box and the radiator in order to remove heat from the E-box and reduce its operational temperature.
- Type
- Chapter
- Information
- Introduction to Spacecraft Thermal Design , pp. 165 - 262Publisher: Cambridge University PressPrint publication year: 2020