Study of deployable lightweight structures for space applications

The growing needs in telecommunications require the development of large parabolic reflectors. A new conceptual design for the architecture of a deployable antenna is therefore proposed in partnership with the CNES. The design of its framework is based on a review of solutions which leads to scissor mechanisms associated with flexible joints. Numerical modelings with finite elements are first developed to simulate the deployment by the release of the energy stored in the joints after the folding. An experimental prototype with a gravity compensation device is then realized. Tests and measurements are performed to characterize the static and dynamic behavior and compared with the results of simulations. Shaping of the reflective surface by a net of cables is then studied. A new form-finding method for obtaining a net with a uniform tension is then proposed. It is applied to different parabolic typologies of nets and the error due to surface faceting is evaluated. The process of net attachment on the antenna rim structure is also treated.

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Source https://theses.hal.science/tel-00761365
Author Morterolle, Sébastien
Maintainer CCSD
Last Updated June 2, 2026, 02:00 (UTC)
Created June 2, 2026, 02:00 (UTC)
Identifier tel-00761365
Language fr
Rights https://about.hal.science/hal-authorisation-v1/
contributor Conception en structures (CS) ; Laboratoire de Mécanique et Génie Civil (LMGC) ; Université de Montpellier (UM)-Centre National de la Recherche Scientifique (CNRS)-Université de Montpellier (UM)-Centre National de la Recherche Scientifique (CNRS)
creator Morterolle, Sébastien
date 2011-10-18T00:00:00
harvest_object_id dfb5cc01-f1bc-49fd-8ffb-d0065ddd62be
harvest_source_id 3374d638-d20b-4672-ba96-a23232d55657
harvest_source_title test moissonnage SELUNE
metadata_modified 2026-01-05T00:00:00
set_spec type:THESE