PD CEN/CLC/TR 17603-31-05:2021 - Page 12

Space Engineering. Thermal design handbook. Structural Materials: Metallic and Composite | Status: Current

1 Scope In this Part 5 of the spacecraft thermal control and design data handbooks, clause 4 contains technical data on the metallic alloys used in spacecrafts is given: composition, application areas, properties and behaviour from a thermal and thermo-optics point of view, degeneration and aging. All other properties of the metallic alloys are outside the scope of this document. Properties of composite materials combined to form heterogeneous structures are given in clause 5. The Thermal design handbook is published in 16 Parts TR 17603-31-01 Thermal design handbook – Part 1: View factors TR 17603-31-02 Thermal design handbook – Part 2: Holes, Grooves and Cavities TR 17603-31-03 Thermal design handbook – Part 3: Spacecraft Surface Temperature TR 17603-31-04 Thermal design handbook – Part 4: Conductive Heat Transfer TR 17603-31-05 Thermal design handbook – Part 5: Structural Materials: Metallic and Composite TR 17603-31-06 Thermal design handbook – Part 6: Thermal Control Surfaces TR 17603-31-07 Thermal design handbook – Part 7: Insulations TR 17603-31-08 Thermal design handbook – Part 8: Heat Pipes TR 17603-31-09 Thermal design handbook – Part 9: Radiators TR 17603-31-10 Thermal design handbook – Part 10: Phase – Change Capacitors TR 17603-31-11 Thermal design handbook – Part 11: Electrical Heating TR 17603-31-12 Thermal design handbook – Part 12: Louvers TR 17603-31-13 Thermal design handbook – Part 13: Fluid Loops TR 17603-31-14 Thermal design handbook – Part 14: Cryogenic Cooling TR 17603-31-15 Thermal design handbook – Part 15: Existing Satellites TR 17603-31-16 Thermal design handbook – Part 16: Thermal Protection System