Ceramic tiles provide lightweight, reusable insulation for spacecraft thermal protection systems but are vulnerable to orbital debris impact damage. Because a wide range of impact conditions that may be experienced in orbit cannot be duplicated in the laboratory, design for orbital debris impact effects must include analytical or numerical modeling. Recent research has developed and validated a new computational approach to the simulation of orbital debris impact on porous ceramic thermal protection systems. Simulations using the validated formulation suggest scaling rules for application in spacecraft design.


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    Titel :

    Simulation of Orbital Debris Impact on Porous Ceramic Tiles


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.07.2014




    Medientyp :

    Aufsatz (Konferenz) , Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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    Son, K.J. / Fahrenthold, E.P. / American Institute of Aeronautics and Astronautics; American Society of Mechanical Engineers; American Society of Civil Engineers | British Library Conference Proceedings | 2013


    Simulation of Orbital Debris Impact on Porous Ceramic Tiles

    Son, Kwon Joong / Fahrenthold, Eric P. | AIAA | 2013




    AIAA-2006-2221 Orbital Debris Shape and Orientation Effects on Impact Damage to Shuttle Tiles

    Evans, S. / Williamsen, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006