The thrust produced by a solar sail is a direct function of its attitude. Thus, solar sail thrust vector control is a key technology that must be developed for sailcraft to become a viable form of deep-space transportation. The solar sail community has been studying various sail Attitude Control System (ACS) actuator designs for near Earth orbit as well as deep space missions. These actuators include vanes, spreader bars, two-axis gimbals, floating/locking gimbals with wheels, and translating masses. This paper documents the various concepts and performs an assessment at the highest level. This paper will only compare the various ACS actuator concepts as they stand at the publication time. This is not an endorsement of any particular concept. As concepts mature, the assessments will change.


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    Titel :

    Solar Sail Control Actuator Concepts


    Beteiligte:
    David Mangus (Autor:in) / Andy Heaton (Autor:in)

    Kongress:

    Solar Sail Technology and Applications Conference ; 2004 ; Greenbelt, MD, US


    Erscheinungsdatum :

    05.09.2004


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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