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Azimuthal repositioning of payloads in heliocentric orbit using solar sails

McInnes, C.R. (2003) Azimuthal repositioning of payloads in heliocentric orbit using solar sails. Journal of Guidance, Control and Dynamics, 26 (4). pp. 662-664. ISSN 0731-5090

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    Abstract

    FUTURE solar physics missions will require the ability to reposition multiple spacecraft at different azimuthal positions relative to the Earth, while remaining close to a one year circular orbit. Such azimuthal repositioningwill allow stereoscopicviews of solar features to be generated and will allow imaging of coronal mass ejections as they transit the sun-Earth line. The NASA STEREO mission, which is scheduled for launch in 2005, will utilize two spacecraft to perform such tasks. Both spacecraft will be launched on a Delta II 7925 and will use multiple lunar gravity assists to maneuver the spacecraft onto leading and trailing heliocentric orbits. The two spacecraft will then drift ahead of and behind the Earth on free-drift trajectories,with increasingEarth-sun-spacecraft angles.

    Item type: Article
    ID code: 6240
    Keywords: payloads, guidance systems, space, solar physics, spacecraft, solar sails, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Applied Mathematics, Control and Systems Engineering, Electrical and Electronic Engineering, Space and Planetary Science, Aerospace Engineering
    Subjects: Technology > Mechanical engineering and machinery
    Technology > Motor vehicles. Aeronautics. Astronautics
    Department: Faculty of Engineering > Mechanical and Aerospace Engineering
    Related URLs:
    Depositing user: Strathprints Administrator
    Date Deposited: 12 Jun 2008
    Last modified: 05 Sep 2014 13:33
    URI: http://strathprints.strath.ac.uk/id/eprint/6240

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