The propulsion of an electrostatic solar sail (E Sail) is obtained by extracting momentum from the solar wind through electrostatic repulsion of the positively charged solar wind ions (see Figure 1). The positively charged solar wind protons are deflected by the electric field created around the tethers.This electric field grows in diameter as the spacecraft moves away from the Sun, therefore the E Sail effective area grows. The growth of the E-Sail effective area allows the propulsive force to decrease as 1/r up to distances of 20 AU as it moves away from the Sun, unlike solar sail propulsion whose thrust decreases as 1/r 2 but only to distances of 5AU. This propulsive force is created without using propellant and, therefore, E-sail avoids both the mass and complexity of chemical rockets (that require large amounts of propellant, propellant storage tanks, plumbing, valves, and insulation).


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    Titel :

    Electrostatic Solar Sail: A Propellantless Propulsion Concept for an Interstellar Probe Mission


    Beteiligte:
    DeStefano, Anthony M. (Autor:in) / Wiegmann, Bruce M. (Autor:in) / Bangham, Mike (Autor:in) / Bryan, Thomas (Autor:in) / Carr, John (Autor:in) / Heaton, Andrew (Autor:in) / Johnson, Les (Autor:in) / Tyler, Daniel (Autor:in) / Wright, Kenneth H. Jr. (Autor:in) / Stone, Nobie (Autor:in)

    Kongress:

    American Geophysical Union Fall Meeting ; 2019 ; San Francisco, CA, United States


    Erscheinungsdatum :

    2019-12-09


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






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