PD CEN/CLC/TR 17603-31-03:2021 PDF

1   Scope Factors affecting the equilibrium temperature of a spacecraft surface are described in this Part 3 using simple geometrical configurations and basic assumptions. Methods for conducting calculations on the affect of Solar, planetary and albedo radiation are given taking into consideration the internal and immediate environmental factors and incorporating the various configurations and dimensions of the constituent parts. 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

TR17603-31-03 Thermal design handbook – Part 3: Spacecraft Surface Temperature

TR17603-31-04 Thermal design handbook – Part 4: Conductive Heat Transfer

TR 17603-31-05 Thermal design handbook – Part 5: Structural Materials: Metallic and Composite ...