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Payload Adapter Made from Fiber-Metal-Laminate Struts

  • Boris Kolesnikov
  • Daniel Stefaniak
  • Johannes Wölper
  • Christian Hühne
Chapter
Part of the Research Topics in Aerospace book series (RTA)

Abstract

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.

Keywords

Carbon Fiber Reinforce Plastic Damage Tolerance Glass Fiber Reinforce Plastic Radial Load Global Buckling 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag Berlin Heidelberg 2013

Authors and Affiliations

  • Boris Kolesnikov
    • 1
  • Daniel Stefaniak
    • 1
  • Johannes Wölper
    • 1
  • Christian Hühne
    • 1
  1. 1.Institute of Composite Structures and Adaptive Systems, Composite DesignDeutsches Zentrum für Luft- und Raumfahrt e.V. (German Aerospace Center)BraunschweigGermany

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