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  • 1
    Online Resource
    Online Resource
    American Geophysical Union (AGU) ; 1996
    In:  Journal of Geophysical Research: Planets Vol. 101, No. E10 ( 1996-10-25), p. 23207-23212
    In: Journal of Geophysical Research: Planets, American Geophysical Union (AGU), Vol. 101, No. E10 ( 1996-10-25), p. 23207-23212
    Abstract: The atmospheric entry of a meteor is quite complex, with the body losing kinetic energy both from atmospheric drag and from mass loss due to aerodynamic heating. Moreover, high pressures on the windward side of the body result in enormous compressive stresses which may exceed the yield strength of the material and cause rapid fragmentation of the meteor. While ablative mass loss is not important for extremely large objects, it must be accurately estimated to correctly predict the trajectories of objects that are several tens of meters in diameter. The current paper describes a computer model which performs calculations of shock layer conditions, accounting for the time varying temperature distribution, radiative cooling of the shocked gases, and blockage of surface heating by ablation products. Application of the model to the well‐known Tunguska Event indicates that the responsible bolide was probably a carbonaceous chondrite, although a stony asteroid or a cometary body cannot be conclusively ruled out.
    Type of Medium: Online Resource
    ISSN: 0148-0227
    Language: English
    Publisher: American Geophysical Union (AGU)
    Publication Date: 1996
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    SSG: 16,13
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  • 2
    Online Resource
    Online Resource
    Springer Science and Business Media LLC ; 1995
    In:  Nature Vol. 375, No. 6533 ( 1995-6), p. 638-639
    In: Nature, Springer Science and Business Media LLC, Vol. 375, No. 6533 ( 1995-6), p. 638-639
    Type of Medium: Online Resource
    ISSN: 0028-0836 , 1476-4687
    RVK:
    RVK:
    RVK:
    Language: English
    Publisher: Springer Science and Business Media LLC
    Publication Date: 1995
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    SSG: 11
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  • 3
    Online Resource
    Online Resource
    American Institute of Aeronautics and Astronautics (AIAA) ; 2011
    In:  Journal of Thermophysics and Heat Transfer Vol. 25, No. 2 ( 2011-04), p. 319-320
    In: Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics (AIAA), Vol. 25, No. 2 ( 2011-04), p. 319-320
    Type of Medium: Online Resource
    ISSN: 0887-8722 , 1533-6808
    Language: English
    Publisher: American Institute of Aeronautics and Astronautics (AIAA)
    Publication Date: 2011
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