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Generally, the development of spacecrafts is costly and time-consuming because the thermal control system and other subsystems of the spacecraft adopt an iterative design until an optimum solution is found. To solve this issue, we proposed an innovative thermal design approach with promising two-phase flow device, oscillating heat pipe.

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This page is a summary of: Thermal and Structural Performance of a Small Satellite with Networked Oscillating Heat Pipes, Journal of Spacecraft and Rockets, February 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35242.
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