Abstract
Large deployable reflectors usually are composed of (metallic) meshes as reflecting surfaces being tensioned via a stiffening structure. In order to overcome the inherent deviation of their shape from the ideal one, a new type of reflecting surface is investigated together with a stiffening structure composed by tensioned membranes. It is made of carbon fibre reinforced silicone generating a double curved non-tensioned shell-membrane. Relevant RF and thermo-mechanical characteristics are presented. The overall reflector concept is also discussed together with first results obtained from scaled laboratory models.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of The European Conference on Antennas and Propagation |
| Subtitle of host publication | EuCAP 2006 |
| State | Published - Oct 2006 |
| Event | European Conference on Antennas and Propagation: EuCAP 2006 - Nice, France Duration: 6 Nov 2006 → 10 Nov 2006 |
Publication series
| Name | European Space Agency, (Special Publication) ESA SP |
|---|---|
| Volume | 626 SP |
| ISSN (Print) | 0379-6566 |
Conference
| Conference | European Conference on Antennas and Propagation: EuCAP 2006 |
|---|---|
| Country/Territory | France |
| City | Nice |
| Period | 6/11/06 → 10/11/06 |
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