Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1717326 | Acta Astronautica | 2006 | 11 Pages |
Abstract
An interplanetary small satellite mission is presented in this paper. The mission is to capture a series of images of a near earth object (NEO) and transmit them back to Earth. In this work, a full design and system description of the satellite is presented along with a simple outline of the mission and the expected imagery received. The aim of the design process was to produce a practical, low-cost, small satellite mission with mainly commercial off-the-shelf components and a rapid development schedule. Despite difficult mass and volumetric constraints, the Prometheus team was able to establish that a small microsatellite observation mission for NEOs appears feasible in the near-term.
Keywords
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
F. Kennedy, I. Coxhill, T. Kormos, E. Imre, J. Fielding, S. Atek, V. Lappas, M. Freebody,