The application provides a high-thermal-
conductivity heat dissipation integrated composite
heat control film for satellites, which comprises a protective layer, a nano
heat control film and a
graphite film. The nano
heat control film comprises a protective layer based on the surface of the film and a three-dimensional micro-nano structure, the
graphite film is packaged by
hot melt adhesive and is pasted together with the nano heat control film by the
hot melt adhesive to form a new high-thermal-
conductivity heat dissipation integrated composite heat control film. The application is pasted on the outer surface of a
satellite cabin plate or an antenna and the like by
silicone rubber, so that the outer surface of the
satellite has the characteristics of
high reflectivity to the solar spectrum, high
emissivity to the
infrared spectrum and high
thermal conductivity, the uniformity of the temperature field of the whole
satellite is improved, the reliability of the single
machine in the cabin is improved, the
production cycle of the product is short and the product is convenient to implement. The application solves the problems of
high heat flux density, complex illumination components and rapid development of future low-
orbit satellite constellations, the production cost is significantly reduced, and the commercial
batch production of the satellite constellations is facilitated.