Ejecta Size Distribution Resulting from Hypervelocity Impacts between Aluminum Alloys

Article Preview

Abstract:

We investigated the effects of impact velocity on ejecta size when aluminum alloy 2017-T4 spheres with a diameter of 3.2 mm impacted aluminum alloy 6061-T6 targets with a thickness of 30 mm at velocities of 2 to 7 km/s. We used a two-stage light-gas gun at the Institute of Space and Astronautical Science (ISAS)/Japan Aerospace Exploration Agency (JAXA). To examine the scattering angles of the ejecta, the following was placed 50 mm in front of the target: a witness plate (150 mm × 150 mm, 2 mm in thickness) made of copper with a hole of 30 mm. The ejection behaviors of fragments were observed using a high-speed video camera. The size distributions of the ejecta were examined in detail. The cumulative number of ejecta was proportional to the square of the impact velocity; in other words, to the impact energy of the projectiles. An experimental formula was created by curve fitting of the cumulative number distribution of the projected areas to a bilinear exponential distribution model when the aluminum alloy spheres struck the aluminum alloy targets.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

338-343

Citation:

Online since:

June 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] O.L. Valerio-Flores, L.E. Murr, V.S. Hernandez and S.A. Quinodes: J. Mater. Sci. Vol. 39 (2004), p.6271.

Google Scholar

[2] V.S. Hernandes, L.E. Murr and I.A. Anchondo: Int. J. Impact Engng. Vol. 32 (2006), p. (1981).

Google Scholar

[3] ISO 11227: 2012, Space systems - Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact (2012).

DOI: 10.3403/30237422

Google Scholar

[4] K. Sugahara, K. Aso, Y. Akahoshi, T. Koura and Y. Narumi: Proc. 60th Int. Astronautical Cong. (2009), IAC-09-A6. 3. 06.

Google Scholar

[5] J.M. Siguier and J.C. Mandeville: Proc. IMechE G Vol. 221 (2007), p.969.

Google Scholar

[6] D. Numata, T. Kikuchi, M. Sun, K. Kaiho and K. Takayama: Proc. 26th Int. Symp. Shock Waves (2007), p.821.

Google Scholar

[7] N. Kawai, K. Tsurui, S. Hasegawa, and E. Sato: Rev. Sci. Instrum. Vol. 81 (2010), 115105.

Google Scholar

[8] M. Nishida, K. Nozaki, K. Hayashi and S. Hasegawa: Proceedings of the 6th European Conference on Space Debris (2013), in press.

Google Scholar

[9] N.L. Johnson, P.H. Krisko, J. -C. Liou, and P.D. Anz-Meador: Adv. Space Res. Vol. 28 (2001), p.1377.

Google Scholar

[10] M. Nishida, K. Kuzuya, K. Hayashi and S. Hasegawa: Int. J. Impact Engng. Vol. 54 (2013), p.161.

Google Scholar

[11] D. E. Grady and M. E. Kipp: J. Appl. Phys. Vol. 58 (1985), p.1210.

Google Scholar