Zobrazeno 1 - 10
of 21
pro vyhledávání: '"I.V. Usovik"'
Autor:
I.V. Usovik, A.I. Nazarenko
Publikováno v:
Acta Astronautica. 204:826-830
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5492a989103452e4730e62ca1d278c1
https://doi.org/10.1016/j.actaastro.2022.09.025
https://doi.org/10.1016/j.actaastro.2022.09.025
Autor:
I.V. Usovik
Publikováno v:
Journal of Space Safety Engineering. 10:55-58
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::781b4042cdcfa222805de621c6b455e4
https://doi.org/10.1016/j.jsse.2022.12.001
https://doi.org/10.1016/j.jsse.2022.12.001
Autor:
A.I. Nazarenko, I.V. Usovik
Publikováno v:
Acta Astronautica. 194:383-389
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d63cb93109a6abc632c093243e5600d8
https://doi.org/10.1016/j.actaastro.2021.12.001
https://doi.org/10.1016/j.actaastro.2021.12.001
Autor:
V.G. Petukhov, I.V. Usovik, N.A. Testoyedov, V. V. Svotina, A.I. Pokryshkin, G. A. Popov, V.A. Kirillov, V. A. Obukhov
Publikováno v:
Acta Astronautica. 194:390-400
The largest population of space debris is observed in the low-Earth-orbit region with altitudes of 600–1000 km and inclinations of 80–100°. As follows from the predictive calculations, space debris removal from this region exactly is of the firs
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5d308b40aaa1433a27355d31563b40b0
https://doi.org/10.1016/j.actaastro.2021.09.041
https://doi.org/10.1016/j.actaastro.2021.09.041
Autor:
V.G. Petukhov, V. A. Obukhov, V.A. Kirillov, G. A. Popov, N.A. Testoyedov, I.V. Usovik, V. V. Svotina
Publikováno v:
Acta Astronautica. 181:569-578
Application of the method of removal of space debris objects by an ion beam - the IBS method - seems to be the most effective for cleaning the GEO region. This is due to the low energy consumption for transfer one object in a safe orbit delta-V≃11
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0cbdef09e211e16aaddd29c09c064a66
https://doi.org/10.1016/j.actaastro.2021.01.043
https://doi.org/10.1016/j.actaastro.2021.01.043
Publikováno v:
Acta Astronautica. 176:598-608
The paper presents results of analysis of existing mathematical models for orbital debris fragments breakup in high velocity collisions. The breakup models are modified and updated taking into account the latest breakup criteria, experimental data an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7e576db51856a32475a3a830f5f633e0
https://doi.org/10.1016/j.actaastro.2020.02.050
https://doi.org/10.1016/j.actaastro.2020.02.050
Autor:
I.V. Usovik, А.I. Nazarenko
Publikováno v:
Acta Astronautica. 163:142-146
The article considers specific examples, which show that the solution of the problem on determining the reentry time of elliptic-orbit satellites can be unstable. An analysis is executed on the basis of orbital data about reentry of two satellites: M
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29c867abd285c7d58cc96834fbe5db58
https://doi.org/10.1016/j.actaastro.2019.01.026
https://doi.org/10.1016/j.actaastro.2019.01.026
Autor:
I.V. Usovik, А.I. Nazarenko
Publikováno v:
Journal of Space Safety Engineering. 6:24-29
The problem under consideration has drawn attention of experts in connection with the events of large-size, dangerous spacecraft reentry. Traditionally, this problem has been solved on the basis of application of the least squares technique. In so do
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1bf908881f58abaaa033d4489707126c
https://doi.org/10.1016/j.jsse.2019.01.002
https://doi.org/10.1016/j.jsse.2019.01.002
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Akademický článek
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