This invention relates to a small, high-precision
temperature control device, belonging to the field of
spacecraft thermal control technology. A cover plate and a base plate form a
closed cavity, which is installed inside the
satellite via a heat insulation pad. The temperature-controlled device is mounted on the base plate inside the
closed cavity via the heat insulation pad. Heaters and temperature sensors are installed on the temperature-controlled device, the base plate of the
temperature control device, and the cover plate, respectively. Depending on the heat dissipation of the temperature-controlled device,
thermal insulation or heat dissipation-enhancing
thermal control coatings are selected between the temperature-controlled device and the
temperature control device, and between the outside of the temperature control device and the
satellite. By setting conditional formulas, the controlled temperature of the object, the controlled temperatures of the cover plate and the base plate, the surface area of the cover plate and the base plate, the designed temperature
control power of the object, and the designed temperature
control power of the cover plate and the base plate are determined, and their rationality is confirmed through parameter
verification. This invention can significantly suppress the influence of
satellite temperature fluctuations on the temperature of the controlled object, achieving high-precision temperature control of the controlled object.