Communications: radio wave antennas – Antennas – Mesh – woven – braided or multiple strip
Patent
1983-08-10
1987-01-06
Lieberman, Eli
Communications: radio wave antennas
Antennas
Mesh, woven, braided or multiple strip
343912, H01Q 1516
Patent
active
046350713
ABSTRACT:
A deployable spacecraft borne circular reflector structure comprises a plurality of plies of graphite fiber reinforced epoxy (GFRE) fibers, each ply comprising at least two layers of graphite epoxy reinforced fibers having quasi-isotropic properties. A circular ring of multiple layer plies of like construction as the reflector and having a U-shaped cross-section is bonded to the reflector rear surface adjacent the reflector peripheral edge. Each layer of each structure is formed from prepreg graphite fiber epoxy reinforced material.
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"Optimized Design and Fabrication Processes for Advanced Composite Spacecraft Structures," by Mazzio et al., 17th Aerospace Sciences Meeting, New Orleans, LA, Jan. 15-17, 1979, p. 2, col. 2, pp. 5-7.
"Advanced Composite Structures for Satellite Systems," by Gounder, RCA Engineer, 26-4, Jan./Feb. 1981, pp. 1, 14-18, 21.
"The SBS Communication Satellite-An Integrated Design," by Rosen, CH1352-4/78/0000-0343, 1978 IEEE, pp. 344-345.
"New Flexible Substrates with Anti-Charging Layers for Advanced Light-Weight Solar Array," by Rusch, Proc. European Symp. on Photovoltaic Generators in Space, Sep. 11-13, 1978, sections 2-4.
Gounder Raj N.
Jacobs Brian D.
Shu Chi-Fan
Lieberman Eli
RCA Corporation
Squire William
Tripoli Joseph S.
Troike Robert L.
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