Solar sails can be classified into two groups based on their method of stabilization: 1) truss supported, and 2) centrifugally (spin) supported. The truss configuration requires masts or booms to deploy, support, and rigidize the sails whereas the spin type uses the spacecraft’s centrifugal force to deploy and stabilize the sails. The truss-supported type sail has a scaling limitation because as the sail area gets larger, the sail is increasingly more difficult to make and stow: the masts and booms get heavier, occupying more volume, and have increased risk during deployment. This major disadvantage limits the size of the sail area. The spin type comes in two configurations: 1) spinning square/disk sail and 2) heliogyro sail. This spinning square/disk sail architecture suffers the same sail area limitation as the truss-supported sail.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Steering Concept of a 2-Blade Heliogyro Solar Sail Spacecraft


    Beteiligte:
    P. Wiwattananon (Autor:in) / R. G. Bryant (Autor:in)

    Erscheinungsdatum :

    2017


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Steering Concept of a 2-Blade Heliogyro Solar Sail Spacecraft

    Wiwattananon, Peerawan / Bryant, Robert G. | NTRS | 2017


    Heliogyro-Configured Solar Sail Spacecraft

    Wiwattananon, Peerawan / Bryant, Robert G. | NTRS | 2015


    Heliogyro-Configured Solar Sail Spacecraft

    P. Wiwattananon / R. G. Bryant | NTIS | 2015


    Heliogyro Solar Sail Blade Twist Control (AAS 12-003)

    Guerrant, D. / Lawrence, D. / Wilkie, W.K. et al. | British Library Conference Proceedings | 2012


    Heliogyro Solar Sail Research at NASA

    Wilkie, W. Keats / Warren, Jerry E. / Horta, Lucas G. et al. | Springer Verlag | 2014