Influence of temperature on crater and ejecta size following hypervelocity impact of aluminum alloy spheres on thick aluminum alloy targets

International Journal of Impact Engineering

Volumn 42, Issue , 2012, Pages 37-47

  Nishida, Masahiro ^a   Hayashi, Koichi ^a   Nakagawa, Junichi ^a   Ito, Yoshitaka ^a  

^a NAGOYA INSTITUTE OF TECHNOLOGY   (Japan)

Author keywords

Cratering; Ejecta fragment; Hypervelocity impact; Temperature effect; Thick target

Indexed keywords

CRATERING; EJECTA FRAGMENT; HYPERVELOCITY IMPACT; TEMPERATURE EFFECT; THICK TARGET;

ALUMINUM; CERIUM ALLOYS; RECTANGULAR WAVEGUIDES; SOLAR SYSTEM; VELOCITY;

ALUMINUM ALLOYS;

EID: 83655164067     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijimpeng.2011.11.006     Document Type: Article

References (26)

1. V.S. Hernandes, L.E. Murr, and I.A. Anchondo Experimental observations and computer simulations for metallic projectile fragmentation and impact crater development in thick metal targets Int J Impact Eng 32 2006 1981 1999
2. O.L. Valerio-Flores, L.E. Murr, V.S. Hernandez, and S.A. Quinodes Observations and simulations of the low velocity-to-hypervelocity impact crater transition for a range of penetrator densities into thick aluminum targets J Mat Sci 39 2004 6271 6289
3. D. Numata, T. Kikuchi, M. Sun, K. Kaiho, and K. Takayama Experiment study of ejecta composition in hypervelocity impact using ballistic range Proc. of Symp. Shock Waves in Japan 2007 221 222
4. D. Numata, T. Kikuchi, M. Sun, K. Kaiho, and K. Takayama Experiment study of ejecta composition in impact phenomenon K. Hannemann, F. Seiler, Proc. 26th Int. Symp. Shock Waves 2007 Springer 821 826
5. Space Systems-Test procedures to evaluate spacecraft material ejecta upon hypervelocity impact (ISO-CD-11227).
6. K. Sugahara, K. Aso, Y. Akahoshi, T. Koura, and T. Narumi Intact measurement of fragments in ejecta due to hypervelocity impact Proc. 60th Int. Astronautical Cong 2009 Daejeon Korea IAC-09-A6.3.06
7. J.M. Siguier, and J.C. Mandeville Test procedures to evaluate spacecraft materials ejecta upon hypervelocity impact Proc. IMechE G vol. 221 2007 SAGE Publications UK 969 974
8. T. Michikami, K. Moriguchi, S. Hasegawa, and A. Fujiwara Ejecta velocity distribution for impact cratering experiments on porous and low strength targets Planetary Space Sci 55 2007 70 88 (Pubitemid 44958834)
9. S. Takasawa, A.M. Nakamura, T. Kadono, M. Arakawa, K. Dohi, and S. Ohno Ejecta size distribution from hypervelocity impact cratering of planetary materials: Implication for dust production process of impact origin European Planetary Science Congress 2010 Abstracts vol. 5 2010 Rome, Italy EPSC2010-179
10. D.E. Grady, and M.E. Kipp Impact failure and fragmentation properties of metals, Sandia Report SAND, Sandia 98-0387 1998
11. A.J. Piekutowski Formation and description of debris clouds produced by hypervelocity impact NASA Contractor Rep 4707 1996
12. L.J. DeChant Validation of a computational implementation of the Grady-Kipp dynamic fragmentation theory for thin metal plate impacts using an analytical strain-rate model and hydrodynamic analogues Mech Mater 37 2005 83 94
13. F.E. Allison, K.R. Becker, and R. Vitali Effects of target temperature on hypervelocity cratering Proceedings of fourth symposium on hypervelocity impact 1960 CD Compilation of Original Hypervelocity Impact Symposia, Southwest Research Institute, San Antonio, TX Eglin Air Forth Base, FL 1 12 May 2008
14. B.M. Corbett Numerical simulations of target hole diameters for hypervelocity impacts into elevated and room temperature bumpers Int J Impact Eng 33 2006 431 440 (Pubitemid 44855409)
15. B.M. Corbett Selecting a best-fit temperature-dependent regression model for thin target HVI data Int J Impact Eng 35 2008 1672 1677
16. D. Numata, K. Ohtani, M. Anyoji, K. Takayama, and M. Sun Experimental study of hypervelocity impacts at low temperatures Shock Waves 18 2008 169 183
17. D. Numata, K. Ohtani, M. Anyoji, K. Takayama, K. Togami, and M. Sun HVI tests on CFRP laminates at low temperature Int J Impact Eng 35 2008 pp.1695 1701
18. A. Francesconi, D. Pavarina, C. Giacomuzzoa, and F. Angrillia Impact experiments on low-temperature bumpers Int J Impact Eng 33 2006 264 272 (Pubitemid 44855393)
19. B.K. Wells Hypervelocity impact tests on coated thermoplastic films at cryogenic and elevated temperatures Int J Impact Eng 33 2006 855 861 (Pubitemid 44855371)
20. Structures and properties of aluminum 1991 Japan Institute of Light Metals Ed. Japan pp. 478 [in Japanese]
21. K.B. Hayashida, and J.H. Robinson Single wall penetration equations, NASA TM-103565 1991 Marshall Space Flight Center pp. 3-5
22. A.J. Watts, and D. Atkinson Dimensional scaling for impact cratering and perforation Int J Impact Eng 17 1995 925 935
23. A. Watts, D. Atkinson, and S. Rieco Dimensional scaling for impact cratering and perforation, NASA CR -188259 1993
24. S. Lieblein, N. Clough, and A.R. McMillan Hypervelocity impact damage characteristics in armored space radiator tubes, NASA TN-D-2472 1964 Glenn Research Center pp. 10-11
25. R. Piacesi, R.H. Waser, and V.C.D. Dawson Temperature-yield strength correlation of the crater size produced in aluminum by the hypervelocity impact of aluminum spheres, Maryland, NOLTR 63-142 1964 pp. 1-3
26. B.A. Myers, W.P. Schonberg, and J.E. Williamsen Temperature effects on bumper hole diameters for impact velocities from 2 to 7 km/sec Int J Impact Eng 29 1-10 2003 487 495