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Jia Yang Wang Yirong Hao Yaxin Zheng Lide (Beijing Institute of Spacecraft Environment Engineering, Beijing 100029)
Published:
Abstract: On the basis of the thermal mathematics model of spacecraft, the flux adjustment method to simulate the given temperature varying speed is introduced in this paper, the simulation results and the application examples are introduced, and the correctness of the thermal mathematics model is proved.
Jia Yang Wang Yirong Hao Yaxin Zheng Lide (Beijing Institute of Spacecraft Environment Engineering, Beijing 100029). The Realization of Temperature Varying Speed in Thermal Vacuum Test[J]. .
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