Mechanisms of failure of aluminium-based Whipple shields under hypervelocity impact: insights from continuum simulations
Author:
Funder
ISRO-IITB Space Technology Cell
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s00707-024-03898-y.pdf
Reference48 articles.
1. Limiting Future Collision Risk to Spacecraft: National Academies Press (2011). https://doi.org/10.17226/13244
2. Whipple, F.L.: Meteorites and space travel. Astron. J. 52, 131 (1947). https://doi.org/10.1086/106009
3. Zukas, J.A.: High Velocity Impact Dynamics. Wiley-Interscience, New York (1990)
4. Meng, S., Taddei, L., Lebaal, N., Roth, S.: Advances in ballistic penetrating impact simulations on thin structures using smooth particles hydrodynamics: a state of the art. Thin-Walled Struct. 159, 107206 (2021). https://doi.org/10.1016/j.tws.2020.107206
5. Wen, K., Chen, X.-W., Lu, Y.-g: Research and development on hypervelocity impact protection using whipple shield: an overview. Defence Technol. 17(6), 1864–1886 (2021). https://doi.org/10.1016/j.dt.2020.11.005
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