With a growing interest in atmospheric entry, descent, and landing research as well as the necessity to empirically test increasingly complicated entry systems, a growing need for a quick and cost-effective method of experimentation is needed. The Hypersonic Configurable Unit Ballistic Experiment is a test and evaluation platform allowing for in-situ research and rapid testing of novel technologies in a re-entry environment. HyCUBE takes the form of a small satellite-sized re-entry vehicle and, with the additional space on board the vehicle, can act as a platform for testing novel guidance and control methodologies.


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    Titel :

    Development of a Low-Cost, Highly Flexible Re-Entry Platform


    Beteiligte:
    J Neumann (Autor:in) / S Gagnon (Autor:in) / A Gardi (Autor:in) / V Twin (Autor:in) / S Vedvik (Autor:in) / D Gebre (Autor:in) / E Longmire (Autor:in) / M Simeni (Autor:in) / M Murbach (Autor:in) / A Salas (Autor:in)

    Kongress:

    American Astronautical Society GN&C Conference ; 2024 ; Breckenridge, CO, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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