Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Vadim V. Bashurov"'
Autor:
Andrey G. Ioilev, Gennady V. Bebrnin, Nikolay V. Lapichev, Sergey A. Mesheryakov, Georgy P. Shlyapnikov, Gennady V. Belov, Piotr N. Kalmykov, Vadim V. Bashurov, Yury N. Bukharev, Oleg N. Polevoi, Anatoly I. Tereshin, Mikhail V. Yakovlev, Amangeldy K. Zhiembetov
Publikováno v:
International Journal of Impact Engineering. 29:357-367
Conceptual study of implementation of a high-porous m aterial 1 ayer as a damper in multi-layered shielding of inhabited modules of the International Space Station (ISS) against hypervelocity space debris was performed using parameters of Columbus -
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5473271c9d51c72a0984fef27a258fda
https://doi.org/10.1016/j.ijimpeng.2003.09.031
https://doi.org/10.1016/j.ijimpeng.2003.09.031
Publikováno v:
International Journal of Impact Engineering. 26:735-744
The problem of reducing the jet penetration capability upon its interaction with the finite-thickness target, due to the erosion of the front region of the jet having perforated through the target, is considered. The experimental examination and the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84f735ffc76035e17ad3310a6e703838
https://doi.org/10.1016/s0734-743x(01)00123-3
https://doi.org/10.1016/s0734-743x(01)00123-3
Publikováno v:
International Journal of Impact Engineering. 20:79-88
KERNEL code is based on the SPH-method (Smoothed Particles Hydrodynamics) and assigned to obtain prompt two- and three-dimensional solutions of perforation and damage of multilayered and multisheet bumpers under high- and hypervelocity impact of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0ed2c390fe96ca6c8d0632b97c8852f9
https://doi.org/10.1016/s0734-743x(97)87481-7
https://doi.org/10.1016/s0734-743x(97)87481-7
Autor:
Gennadi V. Belov, Yuri N. Bukharev, Nikolay V. Lapichev, Georgi S. Smirnov, Gennagi V. Bebenin, Yuli A. Fateev, Vadimir I. Zhukov, Vadim V. Bashurov, Georgy P. Schlyapnikov, Anatoli L. Mikhailov, Andrey G. Ioilev
Publikováno v:
International Journal of Impact Engineering. 20:69-78
Results of three sets of experiments modelling space debris impact to spacecraft shield protection in velocities range of 0.5–6.5 km/s are presented. Numerical simulation in the experiments conditions was performed with the help of 3D code KERNEL b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5c7b5bb224b958757e28c99785e9376
https://doi.org/10.1016/s0734-743x(97)87480-5
https://doi.org/10.1016/s0734-743x(97)87480-5