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    Title :

    Minimum impulse technologies for precision attitude control: Minimum Impulse Thruster (MIT) and Hydrazine milliNewton Thruster (HmNT)


    Contributors:

    Conference:

    DARPA/MTO Workshop: Micro-Thruster Technology for Military Applications


    Publication date :

    2003-05-06


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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