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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    Title :

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


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

    Conference:

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


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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