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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    Title :

    Implementation Options for the PROPEL Electrodynamic Tether Demonstration Mission


    Contributors:
    S. G. Bilen (author) / L. Johnson (author) / B. E. Gilchrist (author) / R. P. Hoyt (author) / C. H. Elder (author) / K. P. Fuhrhop (author) / M. P. Scadera (author) / N. H. Stone (author)

    Publication date :

    2014


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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