Payload Adapter Made from Fiber-Metal-Laminate Struts
Kolesnikov, Boris and Stefaniak, Daniel and Wölper, Johannes and Hühne, Christian (2012) Payload Adapter Made from Fiber-Metal-Laminate Struts. In: Adaptive, Tolerant and Efficient Composite Structures Research Topics in Aerospace. Springer berlin Heidelberg. pp. 263-274. ISBN 978-3642291890 .
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In comparison to other transport systems, launch vehicles are characterized by relatively light but extremely valuable payloads. The launcher’s upper stage structures, e.g. payload adapter and fairing, offer the highest weight saving potential. An effective weight reduction can only be achieved by the combined utilization of high performance materials and adapted construction methods. To improve the structures damage tolerance a new hybrid lay-up has been developed, which combines the properties of both, steel and carbon fiber reinforced plastics (CFRP). This chapter presents a preliminary design of a payload adapter as a framework, which is based on the high performance material properties of unidirectional CFRP-steel-laminates, offering a considerable weight saving potential.
|Document Type:||Book Section|
|Title:||Payload Adapter Made from Fiber-Metal-Laminate Struts|
|Date:||30 June 2012|
|Journal or Publication Title:||Adaptive, Tolerant and Efficient Composite Structures|
|In ISI Web of Science:||No|
|Page Range:||pp. 263-274|
|Publisher:||Springer berlin Heidelberg|
|Series Name:||Research Topics in Aerospace|
|Keywords:||Adapter, Framework, Fiber Metal Laminates|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Structures & Materials|
|Institutes and Institutions:||Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures|
|Deposited By:||Daniel Stefaniak|
|Deposited On:||20 Jun 2012 09:49|
|Last Modified:||20 Jun 2012 09:49|
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