This invention discloses a multi-condition
thermal control structure for flat-panel satellites, including a partitioned orthogonal
heat pipe network, a precision
temperature control universal adaptable
thermal control structure, a dedicated
thermal control module for external equipment (star sensors), multi-layer
thermal insulation components, a graded heating circuit, a
phase change energy storage device, a thermal control white paint
radiant heat dissipation surface, and an intelligent
temperature control and regulation unit. The partitioned orthogonal
heat pipe network separately achieves heat dissipation in
high heat flux areas and isolated
temperature control for individual equipment heat dissipation channels. The pre-embedded
phase change energy storage device is coupled to the orthogonal
heat pipe network, enabling long-distance
heat transfer and storage when the high-power antenna is powered on. Simultaneously, the
phase change energy storage device, relying on the orthogonal heat
pipe network, achieves timely heat dissipation. This invention is rationally designed, combining structural optimization with
intelligent control strategies to achieve efficient heat dissipation for high-power payloads, precise temperature control under multiple conditions, compatibility with various types of equipment, and anti-interference temperature control for external equipment, meeting the temperature stability and uniformity requirements of various key equipment.