Due to their simplicity, low-thrust cold-gas propulsion systems have the potential to provide orbital maneuvering capability for small, micro- and even nano-satellites. Each specific mission where cold gas thrusters will be used places a unique set of requirements on the system. For example, micro- spacecraft with masses of 1 - 50 kg, will require thrust levels for typical orbital maintenance maneuvers of 0.1 - 1OmN.


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    Titel :

    Numerical Study of Cold Gas Micronozzle Flows


    Beteiligte:
    M. S. Ivanov (Autor:in) / G. N. Markelov (Autor:in) / A. D. Ketsdever (Autor:in) / D. C. Wadsworth (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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