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  • Transient study about the heat transfer of sublimator combined with fluid loop

    Paper number

    IAC-13,C2,7,12,x16435

    Author

    Ms. Yuying WANG, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China

    Coauthor

    Mr. Qi ZHONG, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China

    Coauthor

    Dr. Xianwen NING, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China

    Coauthor

    Dr. Jindong LI, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China

    Coauthor

    Mr. Wei LV, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China

    Coauthor

    Mr. Jianyin MIAO, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China

    Coauthor

    Dr. Yan WANG, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China

    Year

    2013

    Abstract
    Sublimator is a good candidate to be used as supplemental heat sink of thermal control system for the spacecraft to reject short period large heat load. In this paper, we analyze the transient work performance of sublimator firstly, then present a detailed transient heat transfer model of a spacecraft pumped fluid loop thermal control system(PFLTCS), which employs sublimator as the supplemental heat rejection device. This paper also presents a model of a simulative fluid loop system(SFLS), which is used to test the sublimator performance instead of the integrated PFLTCS. The transient equations of PFLTCS and SFLS are solved via numerical method. The solutions reveal the transient variation of the key parameters of sublimator and the fluid loop, icluding temperature, feed water mass flow rate, phase change front. In addition, experiment results of a sublimator coupon are also provided to validate the computational results. Experiment results show that the transient model can predict the transient characteristics of sublimator and the fluid loop system during the sublimator startup. The computational results also indicate the transient performances of PFLTCS match the SFLS well.
    Abstract document

    IAC-13,C2,7,12,x16435.brief.pdf

    Manuscript document

    IAC-13,C2,7,12,x16435.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.