A constant outward radial thrust acceleration can be used to reduce the radius of a circular orbit of specified period. Heliocentric circular orbits are designed to match the orbital period of Earth or Mars for various radial thrust accelerations and are defined as synchronous orbits. Minimum-time solar sail orbit transfers to these synchronous heliocentric orbits are presented.


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    Titel :

    Solar Sail Optimal Orbit Transfers to Synchronous Orbits


    Beteiligte:
    R. B. Powers (Autor:in) / V. Coverstone (Autor:in) / J. E. Prussing (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Optimal Solar Sail Orbit Transfers to Synchronous Orbits

    Powers, R. B. / Coverstone, V. L. | Springer Verlag | 2001


    Optimal Solar Sail Orbit Transfers to Synchronous Orbits

    Powers, R. B. / Coverstone, V. L. | Online Contents | 2001


    Solar Sail Optimal Orbit Transfers to Synchronous Orbits (AAS 99-334)

    Powers, R. B. / Coverstone-Carroll, V. / Prussing, J. E. et al. | British Library Conference Proceedings | 2000


    Heliocentric Solar Sail Orbit Transfers with Locally Optimal Control Laws

    Malcolm Macdonald / Colin McInnes / Bernd Dachwald | AIAA | 2007