High energy small body missions using solar sail propulsion
McInnes, Colin and Hughes, Gareth W. and Macdonald, M.; (2006) High energy small body missions using solar sail propulsion. In: Proceedings of the 56th International Astronautical Congress. Curran Associates. ISBN 9781604236484
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A range of mission concepts will be discussed which explore the use of solar sail propulsion for high-energy small body missions. It will be shown that a modest sized solar sail can enable high energy small body sample return from extremely demanding targets, while a larger solar sail can quickly deliver a significant payload to high eccentricity comets. Lastly, it will be shown that potentially hazardous near Earth asteroids can be deflected using kinetic energy impacts by using a solar sail to deliver the impactor to a high-energy retrograde orbit.
Creators(s): |
McInnes, Colin, Hughes, Gareth W. and Macdonald, M. ![]() | Item type: | Book Section |
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ID code: | 6271 |
Keywords: | solar sails, propulsion, mechanical engineering, control systems, guidance systems, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics |
Subjects: | Technology > Mechanical engineering and machinery Technology > Motor vehicles. Aeronautics. Astronautics |
Department: | Faculty of Engineering > Mechanical and Aerospace Engineering Technology and Innovation Centre > Advanced Engineering and Manufacturing |
Depositing user: | Strathprints Administrator |
Date deposited: | 09 Jul 2008 |
Last modified: | 29 Oct 2020 04:46 |
Related URLs: | |
URI: | https://strathprints.strath.ac.uk/id/eprint/6271 |
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