Mini-Magnetospheric Plasma Propulsion (M2P2) seeks the creation of a magnetic wall or bubble (i.e. a magnetosphere) that will intercept the supersonic solar wind which is moving at 300–800 km/s. In so doing, a force of about 1 N will be exerted on the spacecraft by the spacecraft while only requiring a few mN of force to sustain the mini-magnetosphere. Equivalently, the incident solar wind power is about 1 MW while about 1 kW electrical power is required to sustain the system, with about 0.25–0.5 kg being expended per day. This nominal configuration utilizing only solar electric cells for power, the M2P2 will produce a magnetic barrier approximately 15–20 km in radius, which would accelerate a 70–140 kg payload to speeds of about 50–80 km/s. At this speed, missions to the heliopause and beyond can be achieved in under 10 yrs. Design characteristics for a prototype are also described.


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    Titel :

    Mini-magnetospheric plasma propulsion (M2P2): High speed propulsion sailing the solar wind


    Beteiligte:
    Winglee, Robert (Autor:in) / Slough, John (Autor:in) / Ziemba, Tim (Autor:in) / Goodson, Anthony (Autor:in) / Bragg, Mary J. (Herausgeber:in) / El-Genk, Mohamed S. (Herausgeber:in)

    Kongress:

    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - 2000 ; 2000 ; Albuquerque, New Mexico (USA)


    Erschienen in:

    AIP Conference Proceedings ; 504 , 1 ; 962-967


    Erscheinungsdatum :

    19.01.2000


    Format / Umfang :

    6 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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    Mini-Magnetospheric Plasma Propulsion (M2P2): High Speed Propulsion Sailing the Solar Wind

    Winglee, R. / Slough, J. / Ziemba, T. et al. | British Library Conference Proceedings | 2000


    Laboratory testing of the Mini-Magnetospheric Plasma Propulsion (M2P2) prototype

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    Laboratory Testing of the Mini-Magnetospheric Plasma Propulsion (M2P2) Prototype

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