The particularity of the aerospace environment makes products more constrained by space and weight. Therefore, the structural design of aerospace products has stricter requirements in terms of miniaturization and weight reduction. This paper introduces the miniaturization and lightweight design of a space-borne equipment by choosing lightweight materials, reasonable space layout, frame structure with stiffeners; The mechanical simulation, including sinusoidal vibration and random vibration, was carried out to verify the reliability of the structure design through modal analysis and safety margin calculation.


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    Titel :

    Structure Design of a Lightweight and Compact Space-Borne Equipment


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Duan, Baoyan (Herausgeber:in) / Umeda, Kazunori (Herausgeber:in) / Kim, Chang-wan (Herausgeber:in) / Qian, Siyue (Autor:in) / Zhang, Wuwei (Autor:in) / Dai, Fangju (Autor:in)


    Erscheinungsdatum :

    13.07.2022


    Format / Umfang :

    8 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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