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  • Potential Usage of Thermoelectric Generators in Thermal Protection System for Reusable Launch Vehicles (RLV)

    Paper number

    IAC-11,C2,5,11,x10281

    Author

    Mr. Siwei Dong, College of Aerospace and Materials Engineering, National University of Defense Technology, China

    Coauthor

    Prof. Weihua Zhang, National University of Defense Technology, China

    Coauthor

    Prof. Zhongwei Wang, College of Aerospace and Materials Engineering, National University of Defense Technology, China

    Year

    2011

    Abstract
    Traditional TPS only aims to reduce the aerodynamic heat which, however, can be used through energy direct conversion by employing thermoelectric generators (TEGs) embedded in TPS to produce electric power. The purpose of this research was to explore the possibility of the usage of thermoelectric materials in the thermal protection system for reusable launch vehicles, in which way TPS and power supply system can be integrated. However, there are some bottlenecks need to be solved, which will be discussed further and some approaches will also be proposed accordingly.
    Abstract document

    IAC-11,C2,5,11,x10281.brief.pdf

    Manuscript document

    (absent)