Aerospace & Defense & Defense

In accordance with the requirements of the spacecraft mission and the internal and external thermal load to be experienced during the spacecraft's work, various thermal control measures are taken to organize the heat exchange process inside and outside the spacecraft, so as to ensure that the temperature level of all instruments, equipment, organisms and structural components of the spacecraft remains within the specified range throughout the operation period.


The thermal control technology of spacecraft is the same in principle as that of industrial production, but it is special because of the thermal control requirements of spacecraft and the special environmental conditions.

• The spacecraft
  
  PCM - Phase Change Material

  The control of periodic heating equipment can be realized by using the property that phase change material absorbs or exotherms heat during the process of phase change and the temperature remains basi

  Heat insulation material

  Prevent the inflow or outflow of heat

  8400 series cooling powder

  In the universe, air convection cannot be used for heat dissipation, and thermal radiation is mainly used for heat dissipation

  Heating element

  Electric heating is used to maintain the allowable temperature required by the equipment

  9000 Series Thermal Conductive Silicone Rubberpad

  Thermal Conductive Silicone Rubberpad used to heat conduction, filling, sealing and shock absorption
• The plane
  
  PCM - Phase Change Material

  Absorb heat, control the temperature, and keep the temperature at the comfortable temperature that we need