The PROPEL flight mission concept will demonstrate the safe use of an electrodynamic tether for generating thrust. PROPEL is being designed to be a versatile electrodynamic-tether system for multiple end users and to be flexible with respect to platform. As such, several implementation options are being explored, including a comprehensive mission design for PROPEL with a mission duration of six months; a space demonstration mission concept design with configuration of a pair of tethered satellites, one of which is the Japanese H-II Transfer Vehicle; and an ESPA-based system. We report here on these possible implementation options for PROPEL. electrodynamic tether; PROPEL demonstration mission; propellantless propulsion


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    Titel :

    Implementation Options for the PROPEL Electrodynamic Tether Demonstration Mission


    Beteiligte:
    Bilen, Sven G. (Autor:in) / Johnson, Les (Autor:in) / Gilchrist, Brian E. (Autor:in) / Hoyt, Robert P. (Autor:in) / Elder, Craig H. (Autor:in) / Fuhrhop, Keith P. (Autor:in) / Scadera, Michael P. (Autor:in) / Stone, Nobie H. (Autor:in)

    Kongress:

    AIAA Space 2014 Conference ; 2014 ; San Diego, CA, United States


    Erscheinungsdatum :

    2014-08-04


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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