The invention concerns an artificial satellite comprising one face from the North face and the South face supporting at least one main radiator (42, 44) having an outer face turned towards space and an inner face opposite the outer face. The satellite comprises a bearing structure carrying the North face, the South face, the East face and the West face. At least one part (54, 56) of said at least one main radiator (42, 44) protrudes from at least one face from the East face and the West face (36). The inner face of said at least one protruding part (54, 56) is covered with a high infrared emissivity material. The value of the dimension (L54,56) of said at least one protruding part (54, 56) is between 19% and 50% of the value of the distance (Lc) between the East and West faces.
The invention concerns an artificial satellite comprising one face from the North face and the South face supporting at least one main radiator (42, 44) having an outer face turned towards space and an inner face opposite the outer face The satellite comprises a bearing structure carrying the North face, the South face, the East face and the West face At least one part (54, 56) of said at least one main radiator (42, 44) protrudes from at least one face from the East face and the West face (36) The inner face of said at least one protruding part (54, 56) is covered with a high infrared emissivity material The value of the dimension (L54,56) of said at least one protruding part (54, 56) is between 19% and 50% of the value of the distance (Lc) between the East and West faces
SATELLITE ARTIFICIEL
ARTIFICIAL SATELLITE
08.01.2019
Patent
Elektronische Ressource
Französisch
IPC: | B64G Raumfahrt , COSMONAUTICS |