Concept includes three major subsystems; energy source, power converter, and ion thrust chamber; diagram of model which, it is believed, results in engine of minimum weight and simplicity; important factors to consider in design and application; problem areas of individual components.


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    Title :

    Ion rocket engine systems


    Additional title:

    Aero Space Eng


    Contributors:
    Boden, R.H. (author)

    Published in:

    Publication date :

    1959


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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