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  5. Propulsion system characterization for the SPHERES Formation Flight and Docking testbed

Propulsion system characterization for the SPHERES Formation Flight and Docking testbed

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Author(s)
Chen, Allen, 1979-
Advisor(s)
David W. Miller.
Alternative Title
Propulsion system characterization for the Synchronized Position Hold Engage and Reorient Experimental Satellites Formation Flight and Docking testbed
Date Issued
2002
Publisher
Massachusetts Institute of Technology
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.
Includes bibliographical references (p. 183-185).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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M.I.T. theses are protected by
copyright. They may be viewed from this source for any purpose, but
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permission. See provided URL for inquiries about permission.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/82246
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