Fluid loop based temperature control system and satellite
By combining the design of fluid loops and deployable radiators, the problem of limited heat dissipation area for low-Earth orbit satellites has been solved, achieving efficient thermal management and reliability, and adapting to the heat dissipation needs of satellites with multiple heat sources.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- LAN JIAN HONGQING (XIONGAN) SPACE TECHNOLOGY CO LTD
- Filing Date
- 2025-08-29
- Publication Date
- 2026-06-16
AI Technical Summary
The heat dissipation area of high-power modules in low-Earth orbit communication satellites is limited, resulting in low heat transfer efficiency and high cost. Existing passive thermal control methods cannot adjust this, leading to energy waste and long production cycles.
A temperature control system based on a fluid loop is adopted, which combines a single-phase fluid loop with a deployable radiator. The working fluid is driven by a mechanical pump to achieve efficient heat collection and long-distance transmission. The heat dissipation area is expanded by deploying the radiator, and the radiation efficiency is improved by combining a high emissivity coating.
It achieves efficient thermal management, meets the heat dissipation requirements of multi-heat source satellites in extreme environments, and features high reliability, low power consumption, and strong scalability, providing a standardized and modular thermal control solution.
Smart Images
Figure CN224366357U_ABST