Development of a Novel Deployment Hinge Mechanism for a Spacecraft Using Axiomatic Design

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Publisher
Guangdong University of Technology
Issue Date
2011-09
Language
English
Citation

ADME 2011 - International Conference on Advanced Design and Manufacturing Engineering

URI
http://hdl.handle.net/10203/176202
Appears in Collection
ME-Conference Papers(학술회의논문)
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