Article ID Journal Published Year Pages File Type
1717326 Acta Astronautica 2006 11 Pages PDF
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.

Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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