A case study in the design and analysis for a 5.0 m deployable composite antenna

Composites Engineering - Tập 3 - Trang 1007-1013 - 1993
P. Fanning1, L. Hollaway1
1Composite Structures Research Unit, Department of Civil Engineering, University of Surrey, Guildford, Surrey GU2 5XH, UK

Tài liệu tham khảo

Abt, 1989, Deployable precision reflectors, Space Technol, 9, 195 Allemang, 1982, A correlation coefficient for modal vector analysis, 110 Brazzini, 1987, Aerospatiale unfurlable reflector Ewins, 1979, Whys and wherefores of modal testing, J. Soc. Env. Engrs, 18, 3 Fanning, 1993, The deployment analysis of a large space antenna, Int. J. Space Structs, 10.1177/026635119300800307 Freeland, 1983, Survey of deployable antenna concepts, 613 Hollaway, 1986, Developments in Plastics Technology III Itanami, 1988, Fan rib type deployable mesh antenna for satellite use, Acta Astronautica, 17, 561, 10.1016/0094-5765(88)90153-1 Miura, 1989, Concept of the tension truss antenna, AIAA J, 28, 1098, 10.2514/3.25172 Roederer, 1989, Unfurlable satellite antennas: a review, Antenna Telecommunic, 44, 475, 10.1007/BF02995012 Russell, 1991, Development of a large deployable space structure Tsai, 1980 York, 1992, Structural analysis of a joint for deployable space systems