A laboratory experimental program was conducted to determine the amount of fragment debris produced and its size distribution when simulated spacecraft walls are penetrated by hypervelocity projectiles. Two tests were made in which a spacecraft wall was struck with a small steel and an aluminum projectile, respectively. Results show that most of the fragment debris were irregularly shaped flat plates. The fragment data follow a cumulative number distribution law of the form N = am(exp b) where m is fragment mass and a and b are constants. Orbital lifetimes of most of the fragments were very short, being on the order of a few days.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Size Distribution of Fragment Debris Produced by Simulated Meteoroid Impact of Spacecraft Wall


    Beteiligte:
    T Dale Bess (Autor:in)

    Kongress:

    8th Conference on Space Simulation ; 1975 ; Silver Spring, MD, US



    Erscheinungsdatum :

    01.01.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Spacecraft survivability in the meteoroid and debris environment

    Christiansen, Eric L. / Hyde, James L. / Snell, Greg | NTRS | 1992



    Spacecraft survivability in the meteoroid and debris environment

    CHRISTIANSEN, ERIC / HYDE, JAMES / SNELL, GREG | AIAA | 1992


    Design Practices for Spacecraft Meteoroid/Debris (M/D) Protection

    Christiansen, E. / University of Texas at Austin / Lyndon B. Johnson Space Center | British Library Conference Proceedings | 1999