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NEW ROBUST DESIGN GUIDELINE FOR IMPERFECTION SENSITIVE COMPOSITE LAUNCHER STRUCTURES – THE DESICOS PROJECT

Degenhardt, Richard (2014) NEW ROBUST DESIGN GUIDELINE FOR IMPERFECTION SENSITIVE COMPOSITE LAUNCHER STRUCTURES – THE DESICOS PROJECT. European conference on spacecraft structures, materials & environmental testing, 1.-4.Apr. 2014, Braunschweig, Deutschland.

Full text not available from this repository.

Abstract

Space industry demands for reduced development and operating costs. Structural weight reduction by exploitation of structural reserves in composite space and aerospace structures contributes to this aim, however, it requires accurate and experimentally validated stability analysis. Currently, the potential of composite light weight structures, which are prone to buckling, is not fully exploited as appropriate guidelines in the field of space applications do not exist. This paper deals with the state-of-the-art advances and challenges related to coupled stability analysis of composite structures which show very complex stability behaviour. Improved design guidelines for composites structures are still under development. This paper gives a short state-of-the-art and presents a proposal for a future design guideline.

Item URL in elib:https://elib.dlr.de/90351/
Document Type:Conference or Workshop Item (Speech)
Title:NEW ROBUST DESIGN GUIDELINE FOR IMPERFECTION SENSITIVE COMPOSITE LAUNCHER STRUCTURES – THE DESICOS PROJECT
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Degenhardt, RichardDLRUNSPECIFIED
Date:1 April 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Buckling, Composite structures, imperfection sensitivity
Event Title:European conference on spacecraft structures, materials & environmental testing
Event Location:Braunschweig, Deutschland
Event Type:international Conference
Event Dates:1.-4.Apr. 2014
Organizer:DLR
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - HL-Primärstrukturen für Orbitale Systeme
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Structural Mechanics
Deposited By: Degenhardt, Richard
Deposited On:25 Aug 2014 11:15
Last Modified:25 Aug 2014 11:15

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