This paper presents the results of an investigation of the response of window materials to hypervelocity projectile impact. Window impact damage is characterized according to the nature and extent of surface and internal damage. Analysis of the test data indicates that, for single-pane specimens, the extent of the damage to the test specimens can be written as functions of the impact parameters of the original projectile and the geometric and material properties of the projectile/ window system. These functions can be used to perform parameter-sensitivity studies and to evaluate hypothetical design applications and configurations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Response of spacecraft window materials to hypervelocity projectile impact


    Beteiligte:


    Erscheinungsdatum :

    01.02.1991



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Hypervelocity Projectile Technology (D2)

    BISCHER, GREG / CASTLE, MARK | AIAA | 1992


    Hypervelocity projectile technology (D2)

    BISCHER, GREG / CASTLE, MARK | AIAA | 1992


    The D2 hypervelocity projectile program

    Dewar, P. | Tema Archiv | 1995


    Projectile size effects on hypervelocity impact craters in aluminum

    Denardo, B. Pat / Summers, James L. / Nysmith, C. Robert | TIBKAT | 1967