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OverviewThis graduate textbook on optimal spacecraft trajectories demonstrates the theory and applications of using the minimum amount of propellant possible to reach a target destination. The author aims to produce the only comprehensive treatment of various aspects of this topic. It includes problems at the ends of the chapters and some of the appendices. But it is also suitable as a scholarly reference book as it includes recent research from the author and his colleagues. Full Product DetailsAuthor: John E Prussing (University of Illinois)Publisher: Oxford University Press, USA Imprint: Oxford University Press, USA ISBN: 9780191848360ISBN 10: 0191848360 Publication Date: 18 February 2018 Audience: General/trade , General Format: Undefined Publisher's Status: Active Availability: In Print  This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us. Table of ContentsReviewsAuthor InformationJohn Prussing, Professor Emeritus of Aerospace Engineering, University of Illinois John Prussing is Professor Emeritus of Aerospace Engineering at the University of Illnois at Urbana-Champaign. He holds a SB, SM and a ScD in 1967 in aerospace engineering all from MIT, and served as professor of aerospace engineering between 1969 and 2007, and continues to teach part time, including short courses at NASA. He has published over 80 articles and has authored/co-authored three books. Tab Content 6Author Website:Countries AvailableAll regions |
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