Subject: Materials engineering
Year: 2003
Type: Article
Type: PeerReviewed
Title: Mechanical and thermal properties of composite material for anti-hail rockets
Author: Srebrenkoska, Vineta
Author: Dimeski, Dimko
Author: Basoski, Gorgi
Author: Smileski, Rose
Abstract: In this paper the technological treatment for production of a molding compound based on short carbon fibers and ablative phenol- formaldehyde resin for high temperature application is optimized. The characterization of the starting raw materials is performed and molding compounds with different fiber/matrix ratio and different fiber length are obtained. From the different lab-samples molded parts are made by thermocompression. All physical, mechanical and thermal properties of the composites are tested. From the obtained results the optimal fiber/matrix ratio are determined for production molding compound for high temperature application. The obtained mechanical results has justified the application of this composite material in automotive, leasure, military and other industries where high temperature resistance and high mechanical strength is required.
Publisher:
Relation: https://eprints.ugd.edu.mk/2736/
Identifier: oai:eprints.ugd.edu.mk:2736
Identifier: https://eprints.ugd.edu.mk/2736/1/Mechanical%20and%20thermal%20properties%20of%20composite%20material%20for%20anti-hail%20rockets.pdfIdentifier: Srebrenkoska, Vineta and Dimeski, Dimko and Basoski, Gorgi and Smileski, Rose (2003) Mechanical and thermal properties of composite material for anti-hail rockets. Confrence Proceedings, III Conference on Drilling and Blasting.
