CEN/CLC/TC 5

Projekta Nr.LVS CEN/CLC/TR 17603-31-13:2021
NosaukumsFluid loops are used to control the temperature of sensitive components in spacecraft systems in order to ensure that they can function correctly. While there are several methods for thermal control (such as passive thermal insulations, thermoelectric devices, phase change materials, heat pipes and short-term discharge systems), fluid loops have a specific application area. This Part 13 provides a detailed description of fluid loop systems for use in spacecraft. The Thermal design handbook is published in 16 Parts: TR 17603-31-01-31-01 Part 1A Thermal design handbook – Part 1: View factors TR 17603-31-01-31-01 Part 2A Thermal design handbook – Part 2: Holes, Grooves and Cavities TR 17603-31-01-31-01 Part 3A Thermal design handbook – Part 3: Spacecraft Surface Temperature TR 17603-31-01-31-01 Part 4A Thermal design handbook – Part 4: Conductive Heat Transfer TR 17603-31-01-31-01 Part 5A Thermal design handbook – Part 5: Structural Materials: Metallic and Composite TR 17603-31-01-31-01 Part 6A Thermal design handbook – Part 6: Thermal Control Surfaces TR 17603-31-01-31-01 Part 7A Thermal design handbook – Part 7: Insulations TR 17603-31-01-31-01 Part 8A Thermal design handbook – Part 8: Heat Pipes TR 17603-31-01-31-01 Part 9A Thermal design handbook – Part 9: Radiators TR 17603-31-01-31-01 Part 10A Thermal design handbook – Part 10: Phase – Change Capacitors TR 17603-31-01-31-01 Part 11A Thermal design handbook – Part 11: Electrical Heating TR 17603-31-01-31-01 Part 12A Thermal design handbook – Part 12: Louvers TR 17603-31-01-31-01 Part 13A Thermal design handbook – Part 13: Fluid Loops TR 17603-31-01-31-01 Part 14A Thermal design handbook – Part 14: Cryogenic Cooling TR 17603-31-01-31-01 Part 15A Thermal design handbook – Part 15: Existing Satellites TR 17603-31-01-31-01 Part 16A Thermal design handbook – Part 16: Thermal Protection System
Reģistrācijas numurs (WIID)72529
Darbības sfēraFluid loops are used to control the temperature of sensitive components in spacecraft systems in order to ensure that they can function correctly. While there are several methods for thermal control (such as passive thermal insulations, thermoelectric devices, phase change materials, heat pipes and short-term discharge systems), fluid loops have a specific application area. This Part 13 provides a detailed description of fluid loop systems for use in spacecraft. The Thermal design handbook is published in 16 Parts: TR 17603-31-01-31-01 Part 1A Thermal design handbook – Part 1: View factors TR 17603-31-01-31-01 Part 2A Thermal design handbook – Part 2: Holes, Grooves and Cavities TR 17603-31-01-31-01 Part 3A Thermal design handbook – Part 3: Spacecraft Surface Temperature TR 17603-31-01-31-01 Part 4A Thermal design handbook – Part 4: Conductive Heat Transfer TR 17603-31-01-31-01 Part 5A Thermal design handbook – Part 5: Structural Materials: Metallic and Composite TR 17603-31-01-31-01 Part 6A Thermal design handbook – Part 6: Thermal Control Surfaces TR 17603-31-01-31-01 Part 7A Thermal design handbook – Part 7: Insulations TR 17603-31-01-31-01 Part 8A Thermal design handbook – Part 8: Heat Pipes TR 17603-31-01-31-01 Part 9A Thermal design handbook – Part 9: Radiators TR 17603-31-01-31-01 Part 10A Thermal design handbook – Part 10: Phase – Change Capacitors TR 17603-31-01-31-01 Part 11A Thermal design handbook – Part 11: Electrical Heating TR 17603-31-01-31-01 Part 12A Thermal design handbook – Part 12: Louvers TR 17603-31-01-31-01 Part 13A Thermal design handbook – Part 13: Fluid Loops TR 17603-31-01-31-01 Part 14A Thermal design handbook – Part 14: Cryogenic Cooling TR 17603-31-01-31-01 Part 15A Thermal design handbook – Part 15: Existing Satellites TR 17603-31-01-31-01 Part 16A Thermal design handbook – Part 16: Thermal Protection System
StatussStandarts spēkā
ICS grupa49.140