A Passive thermal management scheme is devised while taking various Opto-thermal, Opto-mechanical & space environmental constraints into consideration. The finite element model of the thermal management scheme is established in NX NASTRAN to analyze the design w.r.to the given payload and satellite design parameters. The scheme is based on flexible thermal straps made of copper material. This scheme will help in achieving the desired thermal management while isolating the IDDCA assembly from the external vibrations and loads. The scheme is validated through implementation on the actual IDDCA & measuring the change in temperature w.r.to time at critical locations.
Thermal Management Scheme for SWIR IDDCA Used in Space Payloads
Lect. Notes Electrical Eng.
03.01.2023
7 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Thermal environments for Space Shuttle payloads
NTRS | 1985
|Space Launch System Payloads Thermal Environments
NTIS | 2021
|Thermal environments for Space Shuttle payloads
AIAA | 1985
|Space Station Attached Payloads
NTIS | 1990
|