Improvement in Performance of Shaped Charge using Bimetallic Liner
Santosh N. Ingole, M.J. Rathod, K.M. Rajan, R.K. Sinha, S.K. Nayak, Nair Prakash N.P., V.K. Dixit, S.G. Kulkarni
download PDFAbstract. Shaped charge has been designed by replacing conventional monolithic liner with bimetallic liner to possibly enhance its penetration capability. A shaped charge with bimetallic liner formulated using aluminum as the outer cone and copper as the inner cone with cone angle of 520,liner thickness of 2.4mm and calibre of 60mm. Theoretically predicted performance parameters have been compared with that of experimentally determined such as penetration depth and jet tip / slug velocity. The experimental results are reasonably in good agreement with theoretically predicted values. Penetration depth and tip velocity exhibit 22.5% and 10.67% increase respectively in comparison with shaped charge using copper as monolithic liner.
Keywords
Bimetallic Liner, Monolithic Liner, Penetration Depth, Tip Velocity, Slug Velocity
Published online 7/30/2019, 8 pages
Copyright © 2019 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA
Citation: Santosh N. Ingole, M.J. Rathod, K.M. Rajan, R.K. Sinha, S.K. Nayak, Nair Prakash N.P., V.K. Dixit, S.G. Kulkarni, Improvement in Performance of Shaped Charge using Bimetallic Liner, Materials Research Proceedings, Vol. 13, pp 141-148, 2019
DOI: https://doi.org/10.21741/9781644900338-24
The article was published as article 24 of the book Explosion Shock Waves and High Strain Rate Phenomena
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References
[1] Ernest L Baker, Modeling and optimization of shaped charge liner collapse ad jet formation, Technical Report ARAED-TR-92019, US Army Research Development and Engineering Center, New Jersey USA, 1993.
[2] Robert A Brimmer, Manual for shaped charge design, Report 1248, US Naval Ordnance Test Station China Lake, CA, USA, 1950.
[3] WP Walters and SK Golaski, Hemispherical and conical shaped-charge liner collapse and jet formation, Report BRL-TR-2781, US Army Ballistic Research Laboratory Aberdeen Proving Ground, Maryland, USA, 1987.
[4] David Hasenberg, Consequences of coaxial jet penetration performance and shaped charge design criteria, Thesis – NPS-PH-10-0010 , Naval Postgraduate School, CA, USA , 2010.
[5] Saul Skolnick and Albert Goodman, Energy transfer through a multi-layer liner for shaped charges, US Patent 4498367, Southwest Energy Group Ltd Albequerque N Mex, 1985.
[6] P.Y. Chanteret and A. Lichtenberger, Bimetallic liners and coherence of shaped charge jets, Proc. 15th International Symposium on Ballistics, Jerusalem, Israel, 21-24 May 1995, p.143.
[7] Marinko Ugrcic and Dušan Ugrcic, FEM Techniques in Shaped Charge Simulation, Scientific Technical Review ,2009, LVIX ,1, 26-33.
[8] Autodyn User Manual, Century Dynamics Inc., 2001.
[9] DH Lassila, WP Waiters, DJ Nikkel, Jr., RP Kershaw, Analysis Of Soft Recovered Shaped Charge Jet Particles, Symp. Structures Under Extreme Loading Conditions at 1996 ASMEs Pressure Vessels and Piping Conference, Montreal, Canada July 21-26, 1996 (Lawrence Livermore National Lab USA, Report No. UCRL-JC-123850 Apr 1996). https://doi.org/10.2172/251380
[10] Steven M Buc, Liner materials: resources, processes, properties, costs and applications, SPC-91-282-2, DARPA, Viginia, USA, 1991.