This paper describes the analysis of continuum static aerodynamics of Mars Science Laboratory (MSL) entry vehicle (EV). The method is derived from earlier work for Mars Exploration Rover (MER) and Mars Path Finder (MPF) and the appropriate additions are made in the areas where physics are different from what the prior entry systems would encounter. These additions include the considerations for the high angle of attack of MSL EV, ablation of the heatshield during entry, turbulent boundary layer, and other aspects relevant to the flight performance of MSL. Details of the work, the supporting data and conclusions of the investigation are presented.


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    Titel :

    Hypersonic and Supersonic Static Aerodynamics of Mars Science Laboratory Entry Vehicle


    Beteiligte:

    Kongress:

    30th AIAA Applied Aerodynamics Meeting ; 2012 ; New Orleans, LA, Albania


    Erscheinungsdatum :

    25.06.2012


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Hypersonic and Supersonic Static Aerodynamics of Mars Science Laboratory Entry Vehicle

    A. A. Dyakonov / M. Schoenenberger / J. W. Vannorman | NTIS | 2012


    Hypersonic and Supersonic Static Aerodynamics of Mars Science Laboratory Entry Vehicle

    Dyakonov, Artem / Schoenenberger, Mark / Van Norman, John | AIAA | 2012



    Assessment of the Reconstructed Aerodynamics of the Mars Science Laboratory Entry Vehicle

    Schoenenberger, Mark / Norman, John Van / Karlgaard, Chris et al. | AIAA | 2014


    Assessment of the Reconstructed Aerodynamics of the Mars Science Laboratory Entry Vehicle

    Schoenenberger, Mark / Van Norman, John W. / Dyakonov, Artem A. et al. | NTRS | 2013