MODULE COMPOSITION AND DEPLOYMENT METHOD ON DEPLOYABLE MODULAR-MESH ANTENNA STRUCTURES

Citation
M. Watanabe et al., MODULE COMPOSITION AND DEPLOYMENT METHOD ON DEPLOYABLE MODULAR-MESH ANTENNA STRUCTURES, Acta astronautica, 39(7), 1996, pp. 497-505
Citations number
8
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00945765
Volume
39
Issue
7
Year of publication
1996
Pages
497 - 505
Database
ISI
SICI code
0094-5765(1996)39:7<497:MCADMO>2.0.ZU;2-D
Abstract
A deployable modular-mesh antenna is the concept behind a large space antenna. To ensure reliable deployment, a synchronously deployable tru ss structure forming a curved reflector surface has been developed. Th e proposed antenna's main reflector formed by two types of modules usi ng mesh and cable network maintains a sufficient level of rigidity at deployment and deploys with high reliability. Importance has also been placed on the numerical analyses of cables, the mesh, and the truss s tructures. The truss structure analysis is based on a non-linear finit e element method, rather than on multi-body dynamics, so that elastic motions of all truss members during the deployment can easily be handl ed. (C) 1997 Elsevier Science Ltd.