A T-100-3 Russian Hall plasma thruster, xenon flow control unit (XFCU) and US xenon propellant subsystem developed for the RHETT-1 propulsion system are described. The propellant system includes a pressure regulator, on/off valves, service valve and high/low pressure transducers, built to flight-like standards and assembled onto a mounting plate structure. ...


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    Title :

    Experimental Evaluation of the T100-3 Stationary Plasma Thruster and Xenon Propellant System For The RHETT-1 Program


    Contributors:
    Petrosov, V. (author) / Lasinsky, M. (author) / Vasin, A. (author) / Mueller, J. (author) / Garner, C. E. (author)

    Publication date :

    1996-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






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