Table of Contents Author Guidelines Submit a Manuscript
International Journal of Aerospace Engineering
Volume 2017 (2017), Article ID 1015674, 9 pages
https://doi.org/10.1155/2017/1015674
Research Article

Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure

Hypervelocity Impact Research Center, Harbin Institute of Technology, Harbin 150080, China

Correspondence should be addressed to Runqiang Chi; nc.ude.tih@qrihc

Received 25 October 2016; Revised 25 January 2017; Accepted 20 February 2017; Published 16 April 2017

Academic Editor: Enrico C. Lorenzini

Copyright © 2017 Zhiyuan Zhang et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. J.-C. Liou and N. L. Johnson, “Risks in space from orbiting debris,” Science, vol. 311, no. 5759, pp. 340–341, 2006. View at Publisher · View at Google Scholar · View at Scopus
  2. F. Zuiani and M. Vasile, “Preliminary design of debris removal missions by means of simplified models for low-thrust, many-revolution transfers,” International Journal of Aerospace Engineering, vol. 2012, Article ID 836250, 22 pages, 2012. View at Publisher · View at Google Scholar · View at Scopus
  3. S. Ryan, F. Schaefer, R. Destefanis, and M. Lambert, “A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures,” Advances in Space Research, vol. 41, no. 7, pp. 1152–1166, 2008. View at Publisher · View at Google Scholar · View at Scopus
  4. W. Schonberg, F. Schäfer, and R. Putzar, “Hypervelocity impact response of honeycomb sandwich panels,” Acta Astronautica, vol. 66, no. 3-4, pp. 455–466, 2010. View at Publisher · View at Google Scholar · View at Scopus
  5. E. A. Taylor, J. P. Glanville, R. A. Clegg, and R. G. Turner, “Hypervelocity impact on spacecraft honeycomb: hydrocode simulation and damage laws,” International Journal of Impact Engineering, vol. 29, no. 1, pp. 691–702, 2003. View at Publisher · View at Google Scholar · View at Scopus
  6. M. Higashide, N. Onose, and S. Hasegawa, “Sub-millimeter debris impact damage of unmanned spacecraft structure panel,” Procedia Engineering, vol. 58, pp. 517–525, 2013. View at Google Scholar
  7. K. Nitta, M. Higashide, Y. Kitazawa, A. Tekaba, M. Katayama, and H. Matsumoto, “Response of a aluminum honeycomb subjected to hypervelocity impacts,” Procedia Engineering, vol. 58, pp. 709–714, 2013. View at Google Scholar
  8. P. Kang, S.-K. Youn, and J. H. Lim, “Modification of the critical projectile diameter of honeycomb sandwich panel considering the channeling effect in hypervelocity impact,” Aerospace Science and Technology, vol. 29, no. 1, pp. 413–425, 2013. View at Publisher · View at Google Scholar · View at Scopus
  9. S. Ryan, F. Schaefer, and W. Riedel, “Numerical simulation of hypervelocity impact on CFRP/Al HC SP spacecraft structures causing penetration and fragment ejection,” International Journal of Impact Engineering, vol. 33, no. 1–12, pp. 703–712, 2006. View at Publisher · View at Google Scholar · View at Scopus
  10. M. Wicklein, S. Ryan, D. M. White, and R. A. Clegg, “Hypervelocity impact on CFRP: testing, material modelling, and numerical simulation,” International Journal of Impact Engineering, vol. 35, no. 12, pp. 1861–1869, 2008. View at Publisher · View at Google Scholar · View at Scopus
  11. F. K. Schäfer, S. Ryan, M. Lambert, and R. Putzar, “Ballistic limit equation for equipment placed behind satellite structure walls,” International Journal of Impact Engineering, vol. 35, no. 12, pp. 1784–1791, 2008. View at Publisher · View at Google Scholar · View at Scopus
  12. B. Jia, Z.-T. Ma, W. Zhang, and B.-J. Pang, “Numerical simulation investigation in ballistic limit of Whipple shield structure with Al-foam bumperb,” Material Science and Technology, vol. 18, no. 3, pp. 368–372, 2010. View at Google Scholar · View at Scopus
  13. Z. Zhang, R. Chi, B. Pang, and G. Guan, “A study on the split effect of projectile debris on honeycomb core,” in Proceedings of the 4th International Conference on Sustainable Energy and Environmental Engineering, vol. 53, pp. 766–731, Shenzhen, China, December 2015. View at Publisher · View at Google Scholar
  14. E. L. Christiansen, “Design and performance equations for advanced meteoroid and debris shields,” International Journal of Impact Engineering, vol. 14, no. 1, pp. 145–156, 1993. View at Publisher · View at Google Scholar · View at Scopus
  15. W. P. Schonberg, F. Schäfer, and R. Putzar, “Predicting the perforation response of honeycomb sandwich panels using ballistic limit equations,” Journal of Spacecraft and Rockets, vol. 46, no. 5, pp. 976–981, 2009. View at Publisher · View at Google Scholar · View at Scopus