A technical evaluation of a electron bombardment ion thruster, using inert gases, to be tested in one of the satellites under development by the Brazilian Complete Space Program (MECB) is made. This thruster is intended to be used in the attitude control or orbit transfer of small geostationary satellites.


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    Titel :

    Estudo DA Viabilidade de Testes de Um Micropropulsor Ionico Em Satelites DA MECB (Viability Study of Ionic Microthruster Tests on MECB Satellite)


    Beteiligte:
    G. M. Sandonato (Autor:in) / A. M. Filho (Autor:in) / G. O. Ludwig (Autor:in) / J. L. Ferreira (Autor:in) / J. G. Ferreira (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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