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<article article-type="research-article" dtd-version="1.3" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xml:lang="ru"><front><journal-meta><journal-id journal-id-type="publisher-id">radioelectronics</journal-id><journal-title-group><journal-title xml:lang="ru">Известия высших учебных заведений России. Радиоэлектроника</journal-title><trans-title-group xml:lang="en"><trans-title>Journal of the Russian Universities. Radioelectronics</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1993-8985</issn><issn pub-type="epub">2658-4794</issn><publisher><publisher-name>Saint Petersburg Electrotechnical University</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.32603/1993-8985-2022-25-6-50-60</article-id><article-id custom-type="elpub" pub-id-type="custom">radioelectronics-694</article-id><article-categories><subj-group subj-group-type="heading"><subject>Research Article</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="ru"><subject>ЭЛЕКТРОДИНАМИКА, МИКРОВОЛНОВАЯ ТЕХНИКА, АНТЕННЫ</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>ELECTRODYNAMICS, MICROWAVE ENGINEERING, ANTENNAS</subject></subj-group></article-categories><title-group><article-title>Математическая модель бортовой антенны возвращаемых космических аппаратов с учетом поверхностных волн</article-title><trans-title-group xml:lang="en"><trans-title>Mathematical Model of the On-Board Antenna of Reentry Spacecraft Taking into Account Surface Waves</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0002-1441-8032</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Михайлов</surname><given-names>В. Ф.</given-names></name><name name-style="western" xml:lang="en"><surname>Mikhailov</surname><given-names>V. F.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Михайлов Виктор Федорович – доктор технических наук (1986), профессор (1988), почетный работник высшего профессионального образования (2006)</p><p>ул. Б. Морская, д. 67, Санкт-Петербург, 190000</p></bio><bio xml:lang="en"><p>Victor F. Mikhailov, Dr Sci. (Eng.) (1986), Professor (1988), honorary worker of the higher school (2006)</p><p>67, B. Morskaya St., St Petersburg 190000</p></bio><email xlink:type="simple">vmikhailov@pochta.tvoe.tv</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0001-5165-0685</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Мажник</surname><given-names>И. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Mazhnik</surname><given-names>I. V.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Мажник Илья Валерьевич – магистр (2021) по направлению "Инфокоммуникационные технологии и системы связи"</p><p>ул. Б. Морская, д. 67, Санкт-Петербург, 190000</p></bio><bio xml:lang="en"><p>Ilya V. Mazhnik, Master in "Infocommunication Technologies and Communication Systems" (2021)</p><p>67, B. Morskaya St., St Petersburg 190000</p></bio><email xlink:type="simple">ilya.mazhnik@yandex.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Санкт-Петербургский государственный университет аэрокосмического приборостроения</institution><country>Россия</country></aff><aff xml:lang="en"><institution>Saint Petersburg State University of Aerospace Instrumentation</institution><country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2022</year></pub-date><pub-date pub-type="epub"><day>28</day><month>12</month><year>2022</year></pub-date><volume>25</volume><issue>6</issue><fpage>50</fpage><lpage>60</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Михайлов В.Ф., Мажник И.В., 2022</copyright-statement><copyright-year>2022</copyright-year><copyright-holder xml:lang="ru">Михайлов В.Ф., Мажник И.В.</copyright-holder><copyright-holder xml:lang="en">Mikhailov V.F., Mazhnik I.V.</copyright-holder><license xml:lang="ru" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>Данная работа распространяется под лицензией Creative Commons Attribution 4.0.</license-p></license><license xml:lang="en" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>This work is licensed under a Creative Commons Attribution 4.0 License.</license-p></license></permissions><self-uri xlink:href="https://re.eltech.ru/jour/article/view/694">https://re.eltech.ru/jour/article/view/694</self-uri><abstract><sec><title>Введение</title><p>Введение. Бортовые антенны возвращаемых гиперзвуковых летательных аппаратов являются слабонаправленными, что достигается излучением из открытого конца волновода. При прохождении плотных слоев атмосферы они подвергаются аэродинамическому нагреву, для зашиты от которого применяется нагревостойкая радиопрозрачная теплозащита. Случай однородной теплозащиты антенны можно интерпретировать как отсутствие нагрева или нагрев равномерный по толщине теплозащиты.</p></sec><sec><title>Цель работы</title><p>Цель работы. Решается задача о получении аналитического описания характеристик излучения круглого волновода, закрытого плоской однородной диэлектрической пластиной. Поскольку в такой постановке приходится рассматривать резонансную область, то требуется строгое решение уравнений Максвелла.</p></sec><sec><title>Материалы и методы</title><p>Материалы и методы. Из известных аналитических методов решения возможно применение метода интегральных преобразований и метода собственных функций. Оба метода и использованы в работе. При этом использовано предположение, что электрические параметры диэлектрической пластины (теплозащиты) и геометрические размеры не зависят от времени.</p></sec><sec><title>Результаты</title><p>Результаты. Получены соотношения, описывающие диаграмму направленности круглого волновода с диэлектрической теплозащитой и учитывающие электрические параметры теплозащиты и ее толщину. Также получены выражения для полей боковых, поверхностных и вытекающих волн, которые позволяют рассчитать мощность, отводимую этими полями. Получены соотношения для разделения особых точек подынтегральных выражений на полюсы, отвечающие поверхностным, вытекающим и боковым волнам, способным оказывать определенное влияние на диаграмму направленности. Для этого вывода получены аналитические соотношения для определения полюсов подынтегральных выражений, полностью описывающих поверхностные, вытекающие и боковые волны. По некоторым из полученных соотношений были проведены численные расчеты.</p></sec><sec><title>Заключение</title><p>Заключение. Результаты показали, что мощность боковых волн равна нулю. Также из проведенных расчетов следует, что поле излучения поверхностных и вытекающих волн отсутствует, т. е. нет их вклада в диаграмму направленности. </p></sec></abstract><trans-abstract xml:lang="en"><sec><title>Introduction</title><p>Introduction. The onboard antennas of the returned hypersonic aircraft are weakly directional, which is achieved by radiation from the open end of the waveguide. When passing through dense layers of the atmosphere, they are exposed to aerodynamic heating, for protection from which a heat-resistant radio-transparent thermal protection is used. The case of uniform thermal protection of the antenna can be interpreted as the absence of heating or heating uniform in the thickness of the thermal protection.</p></sec><sec><title>Aim</title><p>Aim. The problem of obtaining an analytical description of the radiation characteristics of a circular waveguide closed by a flat homogeneous dielectric plate is solved. Since in such a formulation it is necessary to consider the resonant domain, a strict solution of Maxwell's equations is required.</p></sec><sec><title>Materials and methods</title><p>Materials and methods. Of the known analytical methods of solution, it is possible to use the method of integral transformations and the method of eigen functions. Both of these methods are used in the work. In this case, the assumption is used that the electrical parameters of the dielectric plate (thermal protection) and the geometric dimensions do not depend on time.</p></sec><sec><title>Results</title><p>Results. The relations describing the directional pattern of a circular waveguide with dielectric thermal protection and taking into account the electrical parameters of thermal protection and its thickness are obtained. Expressions are also obtained for the fields of lateral, surface and outflow waves, from which it is possible to calculate the power output by these fields. Relations for the separation of singular points of integrand expressions into poles corresponding to surface, outflow and lateral waves are obtained. Surface, outflow and lateral waves can have a certain effect on the radiation pattern. To determine this conclusion, analytical relations are obtained for determining the poles of integrand expressions that fully describe surface, outflow and side waves. All the analytical results obtained correspond to Numerical calculations were carried out on some of the obtained ratios.</p></sec><sec><title>Conclusion</title><p>Conclusion. The results showed that the power of the side waves is zero. It also follows from the calculations carried out that there is no radiation field of surface and outgoing waves, i.e. there is no contribution of them to the radiation pattern.</p></sec></trans-abstract><kwd-group xml:lang="ru"><kwd>круглый волновод</kwd><kwd>однородная теплозащита</kwd><kwd>поверхностные волны</kwd><kwd>потери электромагнитной энергии</kwd></kwd-group><kwd-group xml:lang="en"><kwd>circular waveguide</kwd><kwd>uniform heat protection</kwd><kwd>surface waves</kwd><kwd>efficiency</kwd></kwd-group></article-meta></front><back><ref-list><title>References</title><ref id="cit1"><label>1</label><citation-alternatives><mixed-citation xml:lang="ru">Meseguer J., Perez-Grande I., Sanz-Andres A. Thermal protection systems // Spacecraft Thermal Control. 2012. P. 305–325. doi: 10.1533/9780857096081.305</mixed-citation><mixed-citation xml:lang="en">Meseguer J., Perez-Grande I., Sanz-Andres A. Thermal Protection Systems. 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