Abstract It is shown that electrodynamic forces play a crucial role in the orbital dynamics of the small Al2O3 particles that are injected into the terrestrial magnetosphere during solid rocket propellent burns. Due to the simplified model that is used to describe the plasma distribution in the magnetosphere, the present results are necessarily preliminary. Even so, it appears that the smallest particles (a = 0.1 μm) will be rapidly eliminated from the magnetosphere. Evaluation of the fate of the somewhat larger (a = 1 μm) particles awaits the construction of a more complete and realistic model of the magnetospheric plasma.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Space debris: Electrodynamic effects


    Contributors:
    Horanyi, M. (author) / Mendis, D.A. (author)

    Published in:

    Publication date :

    1987-01-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Space debris - Electrodynamic effects

    Horanyi, M. / Mendis, D. A. | NTRS | 1986





    Study on electrodynamic tether system for space debris removal

    Ishige, Yuuki / Kawamoto, Satomi / Kibe, Seishiro | Elsevier | 2004