Effect of Heat Sinks on Visco-Elastic & Mechanical Properties of EPDM Based Ablative Composites

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Ablative composites are heat shielding, protective materials that are being used in aerospace industry to protect inner hardware and sensitive devices. The aero dynamic vehicles have to face high stresses, ultra high temperature and adverse conditions of air friction. It is required to develop the materials with light weight and high modulus. EPDM, being heat and ozone attack resistant is the best candidate for the preparation of ablative composites by introducing different heat sinks such as silica, glass fiber, carbon fiber, asbestos, carbon and their combinations have been studied in this work. The prepared materials were tested and it was found that visco elastic behavior of the composites affected by the addition of reinforcing filler (carbon, silica), semi-reinforcing filler (carbon fiber, glass fiber) and non-reinforcing filler (asbestos powder). Mechanical properties tested at different rates, revealed the improvement in tensile strength and % elongation in case of reinforcing and semi-reinforcing fillers but showed adverse effect in case of non-reinforcing fillers. Rheological investigations of these novel composites shows that moony viscosity of the materials containing glass fiber, carbon fiber, silica decreases in the order glass fiber > carbon fiber > silica.

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52-58

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June 2010

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© 2010 Trans Tech Publications Ltd. All Rights Reserved

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[1] M. B. Khan. Polym-Plast. Technol. Eng., 35(1), (1996) pp.187-206.

Google Scholar

[2] Jia Xiaolong et. al., J. Appl. Polym. Sci., 113 (2009) pp.283-289.

Google Scholar

[3] Ju. Lu. Hoon, Stephen Michielgen, J. polym. Sci., 45(3) (2006) pp.253-261.

Google Scholar

[4] W Jon Martin, Griese Richard, US Patent 5212944 published 25 May, (1993).

Google Scholar

[5] Ge Mingliang, Jia Demin, J. Re-inforced Plastics and Composites 28 (2009) pp.5-16.

Google Scholar

[6] W. H. Allen , Dictionary of Technical Terms for Aerospace Use, NASA, Washington, D.C., (1965).

Google Scholar

[7] F. D. Adams (ed. ), NASA Aeronautical Dictionary, U. S. Government Printing Office, Washington, D.C. (1959).

Google Scholar

[8] R. M. L. Baker and M. W. Makemson, An Introduction to Astrodynamics, Academic Press, New York, (1960).

Google Scholar

[9] Heat Transfer with Thermal Control Applications (M. M Yovanovich, ed). Progress in Astronautics and Aeronautics, Vol. 39, AIAA, New York, (1974).

Google Scholar

[10] C.M. Bhuvaneswari, M.S. Sureshkumar, S.D. Kakade, and Manoj Gupta, Defence Science Journal, Vol. 56 (2006) pp.309-320.

Google Scholar

[11] M. A. Bashir, MS Thesis, School of Chemical and Material Engineering NUST, Islamabad, Pakistan (2009).

Google Scholar

[12] M.A. Bashir, M.B. Khan, Proceedings of IBCAST, 19-21 January, (2009) in press.

Google Scholar

[13] Santanu Datta, A.K. Bhattacharya, S.K. Da, E.G. Kontos and J.M. Wafer, Polymer 37, (1996) pp.2581-2585.

Google Scholar

[14] I.M. Ward, Mechanical Properties of Solid Polymers, Wiley Inter-science, London (1971).

Google Scholar

[15] J.D. Ferry, Viscoelastic Properties of Polymers, John Wiley and Sons, New York, 3rd Edition (1980).

Google Scholar

[16] Composite Materials Hand Book (M. M. Schwartz, ed. ). McGraw-Hill, New York, (1992), p.2112.

Google Scholar

[17] B. E. Pearce, J. Spacecraft, 15(2), (1991) p.599.

Google Scholar

[18] D. H. Morton-Jones. Polymer Processing. Polymer research Group, Chemistry Department. University of Lancaster (1989).

Google Scholar