Abstract This paper deals with the aerodynamic and aerothermodynamic design analysis of a conceptual aeroshape, designed to fit the constraints of VEGA launcher fairing and with the capability to perform an end-to-end mission from launch, orbit keeping, re-entry and landing on conventional runway. Aerodynamic and aerothermodynamic performances of the aeroshape under investigation were evaluated for the whole flight scenario by means of several numerical tools as low-order methods and computational fluid dynamics code. Results are provided in the paper and considered applicable to drive the choice of a more suitable aeroshape for a whole re-entry system development.


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    Titel :

    Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle


    Beteiligte:
    Cinquegrana, D. (Autor:in) / Pezzella, G. (Autor:in) / Catalano, P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.07.2015


    Format / Umfang :

    16 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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