Thermal Control Systems are essential for maintaining the temperature of spacecraft and satellites within operational limits, ensuring the reliability and longevity of onboard instruments and systems. They achieve this through a combination of passive and active techniques, which manage heat transfer between the spacecraft and the extreme environment of space.
Transpiration cooling is a thermal management technique where a coolant is passed through small porous surfaces to absorb heat and cool a structure. This method is effective in high-temperature environments like rocket engines and gas turbines, enhancing performance and material longevity by preventing overheating.