Abstract
The advent of high strength and light weight composite materials and newly developed resin materials have radically changed the concepts of advanced space structure and Armoured vehicles [I]. This high strength - to-weight or modulus-to-weight ratios of composites could also result in lighter structural components with lower operating costs and better maintenance history. Since, most current space structures , unmanned vehicles, aircraft structures and high performance defence vehicles are designed to be robust ; designers have been quick to realize the advantages of this advanced material. In response to this, the United State Army Tank-Automotive Command (TACOM) had been evaluating alternative lighter weight materials such as titanium alloys and ceramic tile/polymer-matrix composites (PMCs) that are currently the only practical possibilities for lighter-weight structural armour applications [2]. The alloys do have disadvantages when a spall liner] is required that there are relatively to fabrication example machining and welding. Although PMCs offer some advantages for example freedom from spalling against chemical threats, a quieter operator environment and a high mass efficiency against ball and fragment ballistic threats. Nevertheless, spall liners have been identified as providing improved protection for the tank crews but they still have a number of problems.
Metadata
Item Type: | Thesis (Masters) |
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Creators: | Creators Email / ID Num. Idris, Abd Halim 2000527048 |
Subjects: | T Technology > TK Electrical engineering. Electronics. Nuclear engineering T Technology > TK Electrical engineering. Electronics. Nuclear engineering > Telecommunication |
Divisions: | Universiti Teknologi MARA, Shah Alam > Faculty of Mechanical Engineering |
Programme: | Master of Science |
Keywords: | Fibre, S-Glass, Armoured, Vehicle |
Date: | 2006 |
URI: | https://ir.uitm.edu.my/id/eprint/27057 |
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