There has been a recent increase in emphasis on small satellite because of their low cost, short development time’s relative simplicity, and cost efficiency. However, these satellites do have drawback. Their small size results in small surface areas which often translate into thermal and power constraint. A satellite basically any object that revolves around a planet in a circular or elliptical orbit path. nanosatellites are satellites that weigh less than 10Kg. These types of satellites are designed and developed to carry payloads that are much smaller and has a life span not more than 1 year generally. The below analysis is done on a Low Earth Orbiting Satellite.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Thermal and Vibrational Analysis of Cubesat



    Erschienen in:

    Applied Mechanics and Materials ; 766-767 ; 1091-1096


    Erscheinungsdatum :

    2015-06-08


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    CubeSat form factor thermal control louvers

    EVANS ALLISON L | Europäisches Patentamt | 2018

    Freier Zugriff


    Thermal Ion Instrumentation for CubeSat Missions

    Earle, G. / Davidson, R. / Perdue, M. et al. | British Library Conference Proceedings | 2010


    CUBESAT FORM FACTOR THERMAL CONTROL LOUVERS

    WILLINGHAM ALLISON L | Europäisches Patentamt | 2017

    Freier Zugriff