Modifying Combined Hemisphere–Cylinder Shaped-Charge Liners to Expand the Velocity Range of the Resulting Compact Elements

The currently used shaped charges with combined hemisphere–cylinder liners allows obtaining compact steel elements with velocities of about 6 km/s. In this work, the possibility of modifying hemisphere–cylinder liners to expand the velocity range of the resulting compact elements was investigated by numerical simulation within the framework of a two-dimensional axisymmetric problem of continuum mechanics. The simulation was carried out for a 100 mm diameter shaped charge with a copper liner. The jet-forming part of the liner had a degressive (decreasing from apex to base) thickness, a hemispherical or semi-ellipsoidal outer surface, and a semi-ellipsoidal or semi-superellipsoidal inner surface. As a result of the calculations, the geometric parameters of the combined liners for the formation of compact elements of maximally possible mass with velocities of $$5{-}9.5$$ km/s were selected. For an element with a velocity of about 9.5 km/s, the mass was about 5 g.

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Publication Details

Journal
Combustion Explosion and Shock Waves
Published
2024-12-01
DOI
https://doi.org/10.1134/s0010508224060121
Primary Topic
Electromagnetic Launch and Propulsion Technology
Type
article
Field-Weighted Citation Impact
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article

Modifying Combined Hemisphere–Cylinder Shaped-Charge Liners to Expand the Velocity Range of the Resulting Compact Elements

И. А. Болотина, С. В. Федоров
Combustion Explosion and Shock Waves
Electromagnetic Launch and Propulsion Technology
article

Modifying Combined Hemisphere–Cylinder Shaped-Charge Liners to Expand the Velocity Range of the Resulting Compact Elements

И. А. Болотина, С. В. Федоров
article en

Abstract

The currently used shaped charges with combined hemisphere–cylinder liners allows obtaining compact steel elements with velocities of about 6 km/s. In this work, the possibility of modifying hemisphere–cylinder liners to expand the velocity range of the resulting compact elements was investigated by numerical simulation within the framework of a two-dimensional axisymmetric problem of continuum mechanics. The simulation was carried out for a 100 mm diameter shaped charge with a copper liner. The jet-forming part of the liner had a degressive (decreasing from apex to base) thickness, a hemispherical or semi-ellipsoidal outer surface, and a semi-ellipsoidal or semi-superellipsoidal inner surface. As a result of the calculations, the geometric parameters of the combined liners for the formation of compact elements of maximally possible mass with velocities of $$5{-}9.5$$ km/s were selected. For an element with a velocity of about 9.5 km/s, the mass was about 5 g.

Combustion Explosion and Shock WavesVol. 60(6)
Bauman Moscow State Technical University (RU)
Openalex Percentile: Top 53%
Electromagnetic Launch and Propulsion Technology
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