Design characteristics of thruster configurations for spacecraft attitude control systems investigated. A standard six engine approach is developed and used as the basis for comparison of different thruster configurations. These methods include cases of both skewed and non-skewed configurations. Simulation results are used as a basis for comparison, critical thruster design factors being given based on an analysis of the data.


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    Titel :

    New thruster configurations for spacecraft attitude control systems


    Beteiligte:

    Kongress:

    Engineering in a changing economy ; 1976 ; Clemson, SC


    Erscheinungsdatum :

    1976-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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