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    Titel :

    Monte Carlo Analysis for Spacecraft Thermal Protection System Design



    Kongress:

    25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA



    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    AIAA Paper 2006-2951-2006-3819


    Anmerkungen:

    Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Monte Carlo Analysis for Spacecraft Thermal Protection System Design

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    Monte Carlo approach to spacecraft transfer function realisation via ERA

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