The unfolding deployment of a shell parabolic reflector
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1995-1278
Reference40 articles.
1. 46,NASAJetPropulsionLaboratory.October 1986.
2. SystemsTechnology-1984.pages 251-270. NASA
3. 1985,December 4-6 1984. NASA-CP-2368,N85-
4. 23813andN85-23840.
5. torReportCR-174861,NASALewisResearchCen
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