#spacecraft_thermal_control
Spacecraft thermal control
Process of keeping all parts of a spacecraft within acceptable temperature ranges
In spacecraft design, the function of the thermal control system (TCS) is to keep all the spacecraft's component systems within acceptable temperature ranges during all mission phases. It must cope with the external environment, which can vary in a wide range as the spacecraft is exposed to the extreme coldness found in the shadows of deep space or to the intense heat found in the unfiltered direct sunlight of outer space. A TCS must also moderate the internal heat generated by the operation of the spacecraft it serves.
Thu 19th
Provided by Wikipedia
This keyword could refer to multiple things. Here are some suggestions: