Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Reliability Based Design Optimization of a CubeSat De-Orbiting Mechanism


    Beteiligte:
    Nikbay, Melike (Autor:in) / Acar, Pinar (Autor:in) / Aslan, Alim (Autor:in)

    Kongress:

    12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference



    Erscheinungsdatum :

    01.01.2012




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    RELIABILITY BASED DESIGN OPTIMIZATION OF A CUBESAT DE-ORBITING MECHANISM

    Nikbay, M. / Acar, P. / Aslan, A. et al. | British Library Conference Proceedings | 2012


    Design and Feasibility of a Polar-Orbiting Gravimetry CubeSat

    Piper, Liam / Sherman, Ellie M. / Neu, Jackson et al. | AIAA | 2025



    2.0808 Microcontroller Design for the Montana EaRth Orbiting Pico-Explorer (MEROPE) Cubesat-class Satellite

    Institute of Electrical and Electronics Engineers | British Library Conference Proceedings | 2002