Overall aerodynamic and aerothermal design considerations for the Hermes space vehicle are summarized and a general methodology for the development of Hermes is outlined. Examples of specific design objectives are given which address the problems of longitudinal stability and vehicle aerodynamic heating.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Concepts Generaux Aerodynamiques-Aerothermiques d'Hermes (General Aerodynamic-Aerothermodynamic Concepts for Hermes)


    Contributors:
    P. Perrier (author) / P. Caupenne (author)

    Publication date :

    1987


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Hermes Aerothermodynamic Concept

    F. Cordie / M. Desloires / J. P. Vaunois | NTIS | 1988



    Hermes Thermal Control Subsystem-Design Concepts

    Moscatelli, Antonio / Ferro, Claudio | SAE Technical Papers | 1990


    Computational Simulation of the Aerothermodynamic Characteristics for the Reentry of HERMES

    Mundt, C. / Monnoyer, F. / Hoeld, R. et al. | British Library Conference Proceedings | 1993


    Huygens probe: aerodynamic and aerothermodynamic design

    Baillion, M. / Taquin, G. | British Library Online Contents | 1995