The use of known information sources to identify trends in the development of methods and technical means for removing space objects from low Earth orbits
Abstract
The intensive development of space activities has led to an increase in the amount of space debris in Earth's orbit. The launch and operation of spacecraft such as satellites, launch vehicles (LVs), and space stations are accompanied by a high probability of various residual materials and debris, such as small fragments and debris resulting from the destruction of LVs or spacecraft [1], remaining in orbit and transforming into space debris objects (SDOs). The accumulation of such objects poses a threat to the safety of space missions and may have long-term negative consequences for future space missions and Earth's satellite infrastructure.
With the increasing number of spacecraft and SDOs, there is a need to develop effective and reliable debris mitigation methods to prevent possible collisions and preserve the space environment. It is already known that one of the most popular ways to remove SDOs from low Earth orbits (LEOs) is their deorbiting with subsequent reentry and burn-up in the Earth's atmosphere [2]. However, determining the most promising trends in the development of these methods and technical devices is a complex task that requires in-depth analysis and study of available information sources.
The aim of this work is to review information sources and identify trends in the development of methods and technical means for removing space objects (SOs) from low Earth orbits (LEOs).
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Дронь Н. М. Пути уменьшения техногенного засорения околоземного космического пространства / Н. М. Дронь, П. Г. Хорольский, Л. Г. Дубовик // Науковий вісник Національного гір-ничого університету. - 2014. - № 3. - С. 125-129.
Голубек А. В. Оптимизация энергетических затрат при ком-бинированном уводе объектов космического мусора с низких околоземных орбит / А. В. Голубек, Н. М. Дронь, Л. Г. Дубовик, Н. В. Поляков // Авиационно-космическая техника и технология. - 2018. - № 7. - С. 5–11.
Аэродинамические системы увода космических объектов / А. П. Алпатов, А. С. Палий, А. Д. Скорик // Техническая механи-ка. - 2015. - № 4. - С. 126-138
InflateSail de-orbit flight demonstration results and follow-on drag-sail applications. Underwood, Craig, et al. s.l.: Acta Astronauti-ca, 2019, Vols. 162, pages 344-358.
Accurate aerodynamic model of membranes in free-molecular flow for deorbit device design / F. Nobuhiro et al. Transactions of the japan society for aeronautical and space sciences, aerospace tech-nology japan. 2019. Vol. 17, no. 2. P. 189–196.
Алпатов А. П. Розробка конструктивної схеми та вибір про-ектних параметрів аеродинамічної системи відведення з орбіти розгінних ступенів ракет-носіїв / А. П. Алпатов, О. С. Палій, О. Д. Скорік // Наука та інновації. - 2017. - Т. 13, № 4. - С. 33-45.
Укрпатент. Укрпатент. URL: https://ukrpatent.org/uk (дата звернення: 18.03.2023).
United states patent and trademark office. United States Patent and Trademark Office. URL: https://www.uspto.gov/ (date of access: 21.03.2023).
Espacenet net patent search. Espacenet net patent search. URL: https://worldwide.espacenet.com/ (date of access: 20.03.2023).
Patentscope. WIPO - World Intellectual Property Organization. URL: https://www.wipo.int/patentscope (date of access: 22.03.2023).
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