Flow control of propellant to an electric thruster is an important parameter in the design of reliable, versatile and cost effective electric propulsion subsystems for spacecraft.


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    Title :

    Evaluation of proportional flow control valves


    Contributors:
    Shortwell, R. (author) / Butler, B. (author) / Bushway, D. (author) / Perini, D. (author) / Gross, S. (author) / Kelly, R. (author)

    Conference:

    36th Joint Propulsion Conference


    Publication date :

    2000-07-16


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






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