Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Novel Hybrid Ablative/Ceramic Heatshield for Earth Atmospheric Re-Entry


    Contributors:

    Conference:

    European Conference; 13th, Spacecraft structures, materials & environmental testing; 13th European conference on spacecraft structures, materials & environmental testing; proceedings; editor: L. Ouwehand ; 2014 ; Braunschweig, Germany



    Publication date :

    2014-01-01


    Size :

    71 pages


    Remarks:

    Held in e-store (RMS)




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Methodology for Optimal Design of a Conformal Ablative Heatshield

    Sidor, Adam T. / Braun, Robert D. / Kennedy, Graeme | AIAA | 2018


    Parametric Study of an Ablative TPS and Hot Structure Heatshield for a Mars Entry Capsule Vehicle

    Langston, Sarah L. / Lang, Christapher G. / Samareh, Jamshid A. | NTRS | 2017


    Parametric Study of an Ablative TPS and Hot Structure Heatshield for a Mars Entry Capsule Vehicle

    Langston, Sarah L. / Lang, Christapher G. / Samareh, Jamshid A. | AIAA | 2017


    On Heatshield Shapes for Mars Entry Capsules

    Prabhu, D. / Saunders, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012


    On Heatshield Shapes for Mars Entry Capsules

    Prabhu, Dinesh / Saunders, David | AIAA | 2012