There is an ever-increasing requirement for smaller and more efficient satellites. Minimizing the size of satellites has its advantages. It equally imposes several challenges in bringing up the satellite from the drawing board to a flight model. This paper focuses on an antenna deployment mechanism that is being developed by a student satellite team from BMS College of Engineering. Antenna deployment mechanisms of similar class satellite programs were referred and a model has been developed and analyzed. Experiments were also conducted on a prototype model to verify the conceptual working of the mechanism.


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    Titel :

    Antenna Deployment Mechanism for a 3U CubeSat Project


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Singh, Daljeet (Herausgeber:in) / Chaudhary, Raghvendra Kumar (Herausgeber:in) / Dev Kumar, Krishna (Herausgeber:in) / Sushir, S. (Autor:in) / Ullas, K. (Autor:in) / Prasad, Komal (Autor:in) / Kumar, Vipul V. (Autor:in)


    Erscheinungsdatum :

    01.03.2023


    Format / Umfang :

    13 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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