Explosive propelling devices are used to test objects of rocket and space technology for resistance to the effects of meteoroids and fragments of space debris. Based on numerical simulation carried out with the use of computational complexes ANSYS/AUTODYN and ERUDIT, the possibilities of obtaining aluminum particles with velocities of up to 16 km/s with the aid of shaped charges with a combined cumulative coating are considered. For achieving this goal, the thickness of the jet-forming part of the coating was built up degressively, with the surfaces limiting it having the shape of the surfaces of a semiellipsoid or a semisuperellipsoid of revolution.
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References
J. L. Hyde, E. L. Christiansen, and J. H. Kerr, Meteoroid and orbital debris risk mitigation in a low Earth orbit satellite constellation, Int. J. Impact Eng., 26, 345–356 (2001).
L. S. Novikov, Impact of Solid Particles of Natural and Artifi cial Origin on Space Apparatuses [in Russian], Universitetskaya Kniga, Moscow (2009).
M. V. Khabibullin, M. N. Krivosheina, and A. Yu. Sammel′, Mathematical modeling of the shock action of fragments of space debris on spacecraft windows, J. Eng. Phys. Thermophys., 92, No. 6, 1501–1508 (2019).
E. Christiansen, Design and performances equations for advanced meteoroid and debris shield, Int. J. Impact Eng., 14, 145–156 (1993).
N. N. Smirnov, A. B. Kiselev, K. A. Kondratyev, and S. N. Zolkin, Impact of debris particles on space structures modeling, Acta Astronaut., 67, 333–343 (2010).
A. J. Cable, Hypervelocity accelerators, in: Ray Kinslow (Ed.), High-Velocity Impact Phenomena, Academic Press, New York and London (1970).
L. A. Merzhievskii, V. M. Titov, Yu. I. Fadeenko, and G. A. Shvetsov, High-speed propelling of solid bodies, Fiz. Goren. Vzryva, 23, No. 5, 77–91 (1987).
S. I. Gerasimov, V. I. Erofeev, A. V. Zubankov, V. A. Kikeev, and V. V. Pisetskii, Mathematical simulation and experimental investigation of a contactless measuring section in the problem on high-velocity ballistic flights, J. Eng. Phys. Thermophys., 94, No. 1, 165–170 (2021).
L. P. Orlenko (Ed.), Physics of Explosion [in Russian], in 2 vols., Vol. 2, Fizmatlit, Moscow (2004).
S. I. Gerasimov, D. V. Malyarov, A. G. Sirotkina, S. A. Kapinos, and A. S. Knyazev, Explosive propelling cumulativetype devices for forming high-speed compact elements, Fiz. Goren. Vzryva, 56, No. 4, 128–136 (2020).
P. V. Kruglov and V. I. Kolpakov, Analysis of influence of metal coatings profile heterogeneity on the high-speed elongated elements shape, Eng. J.: Sci. Innovation, No. 7 (2018); https://doi.org/10.18698/2308-6033-2018-7-1782.
M. Katayama and S. Kibe, Numerical study of the conical shaped charge for space debris impact, Int. J. Impact Eng., 26, 357–368 (2001).
S. V. Fedorov, A. V. Babkin, and S. V. Ladov, On the influence of the magnetic field, created in the coating of a shaped charge, on its penetrating effect, Fiz. Goren. Vzryva, 35, No. 5, 145–146 (1999).
I. V. Zhdanov, A. S. Knyazev, and D. V. Malyarov, Obtaining high-sped compact elements of required mass on proportional change in the size of cumulative devices, Trudy Tomsk. Gos. Univ., Ser. Fiz.-Mat., 276, 193–195 (2010).
V. V. Selivanov, S. V. Fedorov, Ya. M. Nikolskaya, and S. V. Ladov, Compact element formation for the modeling of the high-velocity impacts of particles onto spacecraft materials and construction elements in earth conditions, Acta Astronaut., 135, 34–43 (2017).
I. V. Morenko, Distinctive features of the wave process in the well casing under implosion, J. Eng. Phys. Thermophys., 94, No. 2, 496–502 (2021).
S. V. Fedorov, S. V. Ladov, Ya. M. Nikol′skaya, V. D. Baskakov, M. A. Baburin, A. E. Kurepin, A. A. Gorbunkov, and A. S. Pirozerskii, Formation of a flow of high-speed particles by shaped charges with hemispherical–cylindrical coating of degressive thickness, Fiz. Goren. Vzryva, 53, No. 4, 122–125 (2017).
A. Geille, Numerical model of hypervelocity multistage planar disc explosive launchers, Int. J. Impact Eng., 17, 353–362 (1995).
M. V. Silnikov, I. V. Guk, A. F. Nechunaev, and N. N. Smirnov, Numerical simulation of hypervelocity impact problem for spacecraft shielding elements, Acta Astronaut., 150, 56–62 (2018).
S. V. Fedorov, Determining the depth of penetration of porous projectiles during hyperspeed interaction, Zh. Tekh. Fiz., 77, No. 10, 131–134 (2007).
S. V. Fedorov and Ya. M. Bayanova, Hydrodynamic model for penetration of extended projectiles with consideration of material compressibility, Proc. 25th Int. Symp. on Ballistics, Beijing, China (2010), pp. 1032–1039.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 95, No. 6, pp. 1549–1559, November–December, 2022.
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Fedorov, S.V., Kolpakov, V.I., Vinogradova, E.P. et al. Numerical Analysis of the Explosive Formation of Aluminum Particles at Velocities of Up to 16 km/s with the Use of Combined Cumulative Coatings. J Eng Phys Thermophy 95, 1520–1530 (2022). https://doi.org/10.1007/s10891-022-02620-w
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DOI: https://doi.org/10.1007/s10891-022-02620-w