The phrase "a thermal control system" is correct and usable in written English.
It can be used when discussing systems designed to manage temperature in various applications, such as engineering, electronics, or environmental control.
Example: "The spacecraft is equipped with a thermal control system to maintain optimal temperatures for its instruments."
Alternatives: "temperature regulation system" or "heat management system".
A thermal control system of the nanosatellite at an altitude 600 km with an inclination of 98° is presented.
In this paper, a thermal control system, using loop heat pipe as basic heat transfer elements, was designed for Alpha Magnetic Spectrometer.
It is shown that the predicted coating temperature and thickness of the coating layer compare well with the experimentally obtained results, therefore supporting the use of the model as a real-time basis for design and/or adaptation of a thermal control system for the coating process.
A combined solar and light-emitting diode illumination system and a thermal controlling system was installed and tested.
Technoeconomic analysis of the greenhouse integrated to the designed aquifer coupled cavity flow heat exchanger system (ACCFHES) is also conducted based on the yield of capsicum and chilli crops and compared with those of the greenhouse without any thermal control system and the open field condition yields.
A spacecraft with a passive thermal control system utilizes various thermal control materials to maintain temperatures within safe operating limits.
Two phase mechanical pumped cooling loop is a promising thermal control system, which is just like a heat pipe, to realize heat extraction from energetic electrical equipment efficiently.
Various materials are used to achieve a good "thermal control system" (TCS) of spacecraft.
The thermal resistance of the device and the power level applied to the PCM package are of critical importance for design of a passive thermal control system.
The primary goal of the study is to explore the design and thermal performance of a Hybrid Thermal Control System (H-TCS) that would satisfy the diverse thermal requirements of the different space missions.
Sample temperature was strictly controlled using a dedicated thermal control system, which consisted of four preheating chambers to raise the sample temperature from 2 6°C to 37°C and four reaction chambers to maintain the temperature at 37.3°C during the reaction.
