Combined Effect of Thermal and Mechanical Stresses on the Viscoelastic Properties of a Composite Material for Space Structures View Full Text


Ontology type: schema:Chapter     


Chapter Info

DATE

2004

AUTHORS

V. Issoupov , O. V. Startsev , C. Lacabanne , P. Demont , V. Viel-Ingutmbert , M. Dinguirard , E. F. Nikishin

ABSTRACT

Thermal ageing of polymer-matrix composite materials of any long-life spacecraft in LEO involves evolution of mechanical, thermophysical and morphological properties, especially if the structure operates under external mechanical stress like bending. Behavior of KMU-4l carbon/epoxy composite material under combined effect of thermal profiles and static mechanical loading has been studied in a simulated LEO space environment. Thermal cycling was performed on specimens under bending stress reaching 30.4 % of the material ultimate strength. Specimens subjected to combined thermal and mechanical fatigue were examined in a series of 4 intermediate points with a maximum of 120 cycles. The Dynamic Mechanical Thermal Analysis has been employed to follow the global thermomechanical response of KMU-4l composite. The degradation produced was detected by moisture diffusion analysis, the crack density was estimated at the edges of the specimens using a scanning electron microscope. Effects such as the temperature dependence of material properties and matrix post-curing phenomena are also discussed. The results are compared with the appropriate data obtained on specimens of KMU-4l exposed for up to 1501 days to LEO space environments onboard SALYUT and MIR orbital stations. More... »

PAGES

271-281

Book

TITLE

Protection of Materials and Structures from Space Environment

ISBN

1-4020-1690-5

Identifiers

URI

http://scigraph.springernature.com/pub.10.1007/1-4020-2595-5_22

DOI

http://dx.doi.org/10.1007/1-4020-2595-5_22

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1050014019


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