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The Copernicus projectThe Copernicus spacecraft, to be launched on May 4, 2009, is designed for scientific exploration of the planet Pluto. The main objectives of this exploration is to accurately determine the mass, density, and composition of the two bodies in the Pluto-Charon system. A further goal of the exploration is to obtain precise images of the system. The spacecraft will be designed for three axis stability control. It will use the latest technological advances to optimize the performance, reliability, and cost of the spacecraft. Due to the long duration of the mission, nominally 12.6 years, the spacecraft will be powered by a long lasting radioactive power source. Although this type of power may have some environmental drawbacks, currently it is the only available source that is suitable for this mission. The planned trajectory provides flybys of Jupiter and Saturn. These flybys provide an opportunity for scientific study of these planets in addition to Pluto. The information obtained on these flybys will supplement the data obtained by the Voyager and Galileo missions. The topics covered include: (1) scientific instrumentation; (2) mission management, planning, and costing; (3) power and propulsion system; (4) structural subsystem; (5) command, control, and communication; and (6) attitude and articulation control.
Document ID
19910006739
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Barnstable, Bob
(Illinois Univ. Urbana-Champaign, IL, United States)
Polte, Hans
(Illinois Univ. Urbana-Champaign, IL, United States)
Kepes, Paul
(Illinois Univ. Urbana-Champaign, IL, United States)
Walker, Kevin
(Illinois Univ. Urbana-Champaign, IL, United States)
Jacobs, Jeff
(Illinois Univ. Urbana-Champaign, IL, United States)
Williams, Stephen
(Illinois Univ. Urbana-Champaign, IL, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1990
Publication Information
Publication: Aerospace Vehicle Design, Spacecraft Section. Volume 2: Project Groups 5-7
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
No Number:
Accession Number
91N16052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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