Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    FINITE ELEMENT METHOD FOR ABLATIVE THERMAL PROTECTION SYSTEMS DESIGN FOR ATMOSPHERIC RE-ENTRY VEHICLES (AIAA 2018-5207)


    Beteiligte:

    Kongress:

    AIAA International Space Planes and Hypersonic Systems and Technolgies (Conference)



    Erscheinungsdatum :

    01.01.2018


    Format / Umfang :

    8 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    Finite Element Method for Ablative Thermal Protection Systems Design for Atmospheric Re-Entry Vehicles

    Scigliano, Roberto / De Simone, Valeria / De Stefano Fumo, Mario | AIAA | 2018


    Recent Developments of Ablative Thermal Protection Systems for Atmospheric Entry

    Fahy, William P. / Chang, Andrew / Wu, Hao et al. | AIAA | 2021


    Future Directions for Aerospace GN&C (AIAA 2013-5207)

    Dowdle, J.R. / Hattis, P.D. / Miotto, P. et al. | British Library Conference Proceedings | 2013


    Defining Ablative Thermal Protection System Margins for Planetary Entry Vehicles

    Wright, Michael / Cozmuta, Ioana / Laub, Bernard et al. | AIAA | 2011


    AIAA 2006-0780 An Approximate Ablative Thermal Protection System Sizing Tool for Entry System Design

    Dec, J. A. / Braun, R. D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006