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      Dawn Spacecraft Performance: Resource Utilization and Environmental Effects During an 11-Year Mission

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          Abstract

          Dawn was a deep space science mission to the asteroid belt, using solar electric propulsion and a spacecraft derived from an earth-orbiting communications satellite. Although much of the operational history of the mission has been captured in the literature, this work is intended to gather and highlight underreported issues and lessons that would be of specific interest to future electric propulsion and/or asteroid missions. This paper describes the most significant engineering resources consumed over the course of the mission and the use of redundant hardware and software. Also detailed are thermal, micrometeoroid, radiation, and other environmental effects and anomalies that the Dawn spacecraft experienced. A brief description of the mission and spacecraft hardware is also provided.

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          Most cited references43

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          The Dawn Framing Camera

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            The VIR Spectrometer

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              Collision rates and impact velocities in the main asteroid belt

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                Author and article information

                Journal
                jsr
                Journal of Spacecraft and Rockets
                J. Spacecraft
                American Institute of Aeronautics and Astronautics
                1533-6794
                27 December 2019
                January–February 2020
                : 57
                : 1
                : 147-159
                Affiliations
                California Institute of Technology , Pasadena, California 91109
                Author notes
                [*]

                Chief Engineer, Mars Reconnaissance Orbiter, Spacecraft Operations Systems Engineering (394G), Jet Propulsion Laboratory, 4800 Oak Grove Drive. Member AIAA.

                [†]

                Principal Engineer, Communications Architecture and Operations (337K), Jet Propulsion Laboratory, 4800 Oak Grove Drive.

                [‡]

                Engineering Applications Software Engineer, Avionics Integration, Test and Operation (348E), Jet Propulsion Laboratory, 4800 Oak Grove Drive.

                Article
                A34521 A34521
                10.2514/1.A34521
                c8673764-a4e5-4ddd-a993-2af4e3300894
                Copyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental purposes. All other rights are reserved by the copyright owner. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-6794 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 7 April 2019
                : 10 September 2019
                : 19 October 2019
                Page count
                Figures: 11, Tables: 7
                Funding
                Funded by: Jet Propulsion Laboratoryhttp://dx.doi.org/10.13039/100006196
                Categories
                Full-Length Papers

                Engineering,Physics,Mechanical engineering,Space Physics
                Engineering, Physics, Mechanical engineering, Space Physics

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