Research on the skirt tail explosively formed projectile stable shaping technology
- Authors: Li W.1, Wang X.1, Li W.1, Chen K.1
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Affiliations:
- ZNDY of Ministerial Key Laboratory
- Issue: Vol 57, No 5 (2016)
- Pages: 894-899
- Section: Article
- URL: https://journals.rcsi.science/0021-8944/article/view/159750
- DOI: https://doi.org/10.1134/S0021894416050175
- ID: 159750
Cite item
Abstract
The effect of the arc-cone liner configuration parameters on explosively formed projectile (EFP) flight stability is studied experimentally. The effect of the liner edge structure on the EFP formation is computed numerically. The results show that an EFP formed by a liner whose thickness is 0.046 times the charge caliber has improved flight stability and can perforate a steel armor 0.5 times the charge caliber thick in the case of large stand-off distances. A good tail skirt EFP can be formed by choosing appropriate parameters: the liner-to-charge diameter ratio in the interval 0.96–0.98, the liner edge thickness equal to 0.0020–0.0025 times the charge caliber, and the liner edge chamfer of 45–50°.
About the authors
W. Li
ZNDY of Ministerial Key Laboratory
Author for correspondence.
Email: njustlwb@163.com
China, Nanjing, 210094
X. Wang
ZNDY of Ministerial Key Laboratory
Email: njustlwb@163.com
China, Nanjing, 210094
W. Li
ZNDY of Ministerial Key Laboratory
Email: njustlwb@163.com
China, Nanjing, 210094
K. Chen
ZNDY of Ministerial Key Laboratory
Email: njustlwb@163.com
China, Nanjing, 210094
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