A thermoregulated thermomechanical structure for a focal plane suitable for operating in a space environment is disclosed having an interface for supporting dissipative electronic equipment, the structure being monolithic, metallic and including a radiator and a first two-phase heat-transfer fluid transport cavity, extending within the radiator and providing direct thermal transport between the interface and the radiator. The structure also includes a second cavity encapsulating a phase change material.
STRUCTURE THERMOMÉCANIQUE POUR PLAN FOCAL D'INSTRUMENT D'OBSERVATION SPATIALE
THERMOMECHANICAL STRUCTURE FOR FOCAL PLANE OF A SPACE OBSERVATION INSTRUMENT
THERMOMECHANISCHE STRUKTUR FÜR DIE FOKALEBENE EINES RAUMBEOBACHTUNGSINSTRUMENTS
2024-07-03
Patent
Elektronische Ressource
Französisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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