Výsledky vyhledávání - "A. V. Krestina"

Akademický článek

Analysis of the effectiveness of the de-orbiting devices for small satellite

Autor: G. P. Anshakov, A. V. Krestina, I. S. Tkachenko

Publikováno v: Космические аппараты и технологии, Vol 4, Iss 2, Pp 72-84 (2020)

At present, the use of various methods is proposed for the de-orbit of small satellite, and the most feasible and promising of them are analyzed. The task of evaluating the effectiveness of the de-orbiting system for small satellite is set, in the fr

Externí odkaz: https://doaj.org/article/13e096cd48c64f82bad8dc35f5cb729d

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Determining design characteristics of the de-orbiting system for the small satellite

Autor: I. S. Tkachenko, A. V. Krestina

Publikováno v: XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.

The most promising ways to remove small spacecraft from orbit are considered. Design parameters of various variants of construction of the system of small spacecraft removal from orbits are chosen taking into account limitations. The efficiency of th

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d7474f8bc17ddd8549415946f04bd5e7
https://doi.org/10.1063/5.0036020

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Determination of the main design parameters of cost-effective remote sensing satellite systems at the stage of preliminary design

Autor: S. S. Volgin, S. L. Safronov, V. V. Salmin, I. S. Tkachenko, V. I. Kurenkov, Maksim Ivanushkin, A. A. Yakischik, A. V. Krestina

Publikováno v: Journal of Physics: Conference Series. 1745:012089

This article surveys approaches to the selection of design parameters and modelling the functioning of the remote sensing satellite systems, taking into account the requirements and restrictions on customer resources. The objective of this research i

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::67236ae0a3ed1487b25258c4e167c5b0
https://doi.org/10.1088/1742-6596/1745/1/012089

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Analysis of the possibility of using the system for small satellite de-orbiting based on an aerodynamic stabilizer, taking into account the physical features of the Earth’s upper atmosphere

Autor: Maksim Korovin, I. S. Tkachenko, A V Krestina

Publikováno v: Journal of Physics: Conference Series. 1236:012087

The paper presents an analysis of performance of a satellite de-orbiting system that utilizes a deployable aerodynamic stabilizer for controling the angular motion of a spacecraft in order to ensure the correct orientation of the breaking impulse. Th

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::0c4fa48936bf142bfde91b23adb3e00e
https://doi.org/10.1088/1742-6596/1236/1/012087

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