The contents include: 1) Organization of the Orbiter Entry Aeroheating Working Group; 2) Overview of the Principal RTF Aeroheating Tools Utilized for Tile Damage Assessment; 3) Description of the Integrated Tile Damage Assessment Team Analyses Process; 4) Space Shuttle Flight Support Process; and 5) JSC Applied Aerosciences and CFD Branch Applied Research Interests.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Orbiter Entry Aerothermodynamics Practical Engineering and Applied Research


    Contributors:

    Publication date :

    2009


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Orbiter entry aerothermodynamics

    Ried, R. C. | NTRS | 1985


    Configuration Aerothermodynamics of Entry Vehicles

    Throckmorton, D. A. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research &Development; Fluid Dynamics Panal | British Library Conference Proceedings | 1996


    Aerothermodynamics for Dragonfly's Titan Entry

    Brandis, Aaron / Saunders, David / Allen, Gary et al. | NTRS | 2018


    Aerothermodynamics of blunt body entry vehicles

    Hollis, Brian R. | Online Contents | 2012