Back to Search Start Over

Investigation of aluminium Whipple Shield response to hypervelocity impacts close to ballistic limit between 2.5 and 5 km/s.

Authors :
Olivieri, Lorenzo
Faergestad, Rannveig Marie
Giacomuzzo, Cinzia
Lopresti, Stefano
Pitacco, Giovanni
Francesconi, Alessandro
Cardone, Tiziana
Holmen, Jens Kristian
Borvik, Tore
Source :
Acta Astronautica. Jun2024, Vol. 219, p41-47. 7p.
Publication Year :
2024

Abstract

For impact velocities larger than a threshold velocity of 3 km/s, aluminium Whipple Shields present an enhanced protection capability with respect to monolithic protections with the same areal density. In particular, in the range between 3 and 7 km/s the projectile partially fragments and melts after impacting the bumper; modelling this transition might be complex due to the high number of parameters affecting the collision. In particular, limited data is available in literature with a systematic evaluation of such parameters. In this context, a campaign of 22 experiments was performed to assess the response of aluminium Whipple Shields to normal impacts of aluminium projectiles in the transition range up to 5 km/s. In the tests, the projectile diameter was fixed at 2.9 mm and the bumper thickness and impact velocity were systematically varied respectively at 1, 1.5, and 2 mm and between 2.6 and 5 km/s. Collected data included high-velocity videos of the debris cloud generated by the impacts at both low resolution (for all shots) and high resolution (for 19 out of 22 tests); in addition, for 10 experiments high-resolution images of both the bumper and the wall were acquired after the tests. In this paper, the experimental campaign is described and the main collected results are presented; in particular, the influence of the different impact parameters is discussed. Experimental results are finally compared with numerical simulations conducted with a smoothed particle hydrodynamics method available in IMPETUS Solver. • 22 impact experiments were performed on Aluminium Whipple Shields. • The projectile diameter was fixed at 2.9 mm for all tests. • Bumper thickness and impact velocity varied in the ranges 1–2 mm and 2.6–5 km/s. • The influence of the different impact parameters is discussed. • Experimental results are compared with numerical SPH simulations. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
00945765
Volume :
219
Database :
Academic Search Index
Journal :
Acta Astronautica
Publication Type :
Academic Journal
Accession number :
177316865
Full Text :
https://doi.org/10.1016/j.actaastro.2024.03.009