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.
THERMOMECHANICAL STRUCTURE FOR FOCAL PLANE OF A SPACE OBSERVATION INSTRUMENT
2024-07-11
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS / B33Y ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING , Additive (generative) Fertigung, d. h. die Herstellung von dreidimensionalen [3D] Bauteilen durch additive Abscheidung, additive Agglomeration oder additive Schichtung, z. B. durch 3D- Drucken, Stereolithografie oder selektives Lasersintern |
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