Article ID Journal Published Year Pages File Type
1717445 Acta Astronautica 2006 12 Pages PDF
Abstract

The article addresses engineering activities on a key item of innovative solar sail propulsion technologies: lightweight deployable booms to enfold huge membrane structures in space. Design and analysis aspects are covered besides the description of several verification tasks on engineering models including a successful ground demonstration under simulated zero-g conditions of a solar sail breadboard model, which was funded by ESA and DLR in a common effort. Based on lessons learned proposals for design improvements are made in preparation for a future solar sail flight mission. In a first step towards this goal the deployment technology will be demonstrated in Earth's orbit. The DLR Institute of Composite Structures and Adaptive Systems is involved in the ESA–DLR follow-up project by the provision of the deployable booms made of carbon-fiber reinforced polymers (CFRP) and extremely thin sail segments. Kayser Threde GmbH, Germany has been commissioned as system responsible for the implementation of this project.

Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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