<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE article PUBLIC "-//NLM//DTD JATS (Z39.96) Journal Publishing DTD v1.3 20210610//EN" "JATS-journalpublishing1-3.dtd">
<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="en"><front><journal-meta><journal-id journal-id-type="publisher-id">powder</journal-id><journal-title-group><journal-title xml:lang="en">Powder Metallurgy аnd Functional Coatings (Izvestiya Vuzov. Poroshkovaya Metallurgiya i Funktsional'nye Pokrytiya)</journal-title><trans-title-group xml:lang="ru"><trans-title>Известия вузов. Порошковая металлургия и функциональные покрытия</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1997-308X</issn><issn pub-type="epub">2412-8767</issn><publisher><publisher-name>НИТУ "МИСИС"</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.17073/1997-308X-2023-3-30-37</article-id><article-id custom-type="elpub" pub-id-type="custom">powder-825</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="en"><subject>Refractory, Ceramic, and Composite Materials</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="ru"><subject>Тугоплавкие, керамические и композиционные материалы</subject></subj-group></article-categories><title-group><article-title>High-temperature oxidation of ZrB2–SiC–La2O3 ceramic material produced  via spark plasma sintering</article-title><trans-title-group xml:lang="ru"><trans-title>Особенности высокотемпературного окисления керамического материала ZrB2–SiC–La2O3, полученного искровым плазменным спеканием</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0002-5214-0932</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Кульметьева</surname><given-names>В. Б.</given-names></name><name name-style="western" xml:lang="en"><surname>Kulmetyeva</surname><given-names>V. B.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Валентина Борисовна Кульметьева – к.т.н., доцент кафедры механики композиционных материалов и конструкций (МКМК)</p><p>Россия, 614000, г. Пермь, Комсомольский пр-т, 29</p></bio><bio xml:lang="en"><p>Valentina B. Kulmetyeva – Cand. Sci. (Eng.), Associate Professor, Department of Mechanics of Composite Mate­rials and Structures</p><p>29 Komsomolsky Prosp., Perm 614000, Russia</p></bio><email xlink:type="simple">kulmetevavb@pstu.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0009-0000-0171-2024</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Чувашов</surname><given-names>В. Э.</given-names></name><name name-style="western" xml:lang="en"><surname>Chuvashov</surname><given-names>V. E.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Вячеслав Эдуардович Чувашов – аспирант кафедры МКМК</p><p>Россия, 614000, г. Пермь, Комсомольский пр-т, 29</p></bio><bio xml:lang="en"><p>Vyacheslav E. Chuvashov – PhD student, Department of Mechanics of Composite Materials and Structures</p><p>29 Komsomolsky Prosp., Perm 614000, Russia</p></bio><email xlink:type="simple">slavachuvashov@yandex.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0009-0003-6134-2952</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Лебедева</surname><given-names>К. Н.</given-names></name><name name-style="western" xml:lang="en"><surname>Lebedeva</surname><given-names>K. N.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Ксения Николаевна Лебедева – магистрант кафедры МКМК</p><p>Россия, 614000, г. Пермь, Комсомольский пр-т, 29</p></bio><bio xml:lang="en"><p>Kseniya N. Lebedeva – Master’s Student, Department of Mechanics of Composite Materials and Structures</p><p>29 Komsomolsky Prosp., Perm 614000, Russia</p></bio><email xlink:type="simple">lebedkseni@mail.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0001-5835-9727</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Порозова</surname><given-names>С. Е.</given-names></name><name name-style="western" xml:lang="en"><surname>Porozova</surname><given-names>S. E.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Светлана Евгеньевна Порозова – д.т.н., профессор кафедры МКМК</p><p>Россия, 614000, г. Пермь, Комсомольский пр-т, 29</p></bio><bio xml:lang="en"><p>Svetlana E. Porozova – Dr. Sci. (Eng.), Professor, Department of Mechanics of Composite Materials and Structures</p><p>29 Komsomolsky Prosp., Perm 614000, Russia</p></bio><email xlink:type="simple">sw.porozova@yandex.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0001-7476-9734</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Каченюк</surname><given-names>М. Н.</given-names></name><name name-style="western" xml:lang="en"><surname>Kachenyuk</surname><given-names>M. N.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Максим Николаевич Каченюк – д.т.н., доцент кафедры МКМК</p><p>Россия, 614000, г. Пермь, Комсомольский пр-т, 29</p></bio><bio xml:lang="en"><p>Maksim N. Kachenyuk – Dr. Sci. (Eng.), Associate Professor, Department of Mechanics of Composite Materials and Structures</p><p>29 Komsomolsky Prosp., Perm 614000, Russia</p></bio><email xlink:type="simple">maxxkach@yandex.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Пермский национальный исследовательский политехнический университет</institution><country>Россия</country></aff><aff xml:lang="en"><institution>Perm National Research Polytechnic University</institution><country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2023</year></pub-date><pub-date pub-type="epub"><day>21</day><month>09</month><year>2023</year></pub-date><volume>17</volume><issue>3</issue><fpage>30</fpage><lpage>37</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; НИТУ "МИСИС", 2023</copyright-statement><copyright-year>2023</copyright-year><copyright-holder xml:lang="ru">НИТУ "МИСИС"</copyright-holder><copyright-holder xml:lang="en">НИТУ "МИСИС"</copyright-holder><license xlink:href="https://powder.misis.ru/jour/about/submissions#copyrightNotice" xlink:type="simple"><license-p>https://powder.misis.ru/jour/about/submissions#copyrightNotice</license-p></license></permissions><self-uri xlink:href="https://powder.misis.ru/jour/article/view/825">https://powder.misis.ru/jour/article/view/825</self-uri><abstract><p>The study investigated the influence of La2O3 addition on the oxidation properties of composite ceramics with a composition of 80 vol. % ZrB2 and 20 vol. % SiC. The source materials utilized in this study included zirconium diboride (DPTP Vega LLC., Russia), grade 63C silicon carbide (Volzhsky Abrasive Works JSC, Russia), and lanthanum hydroxide concentrate (Solikamsk Magnesium Plant JSC, Russia), with the following elemental content (wt. %): La – 54.2, Nd – 4.3, Pr – 2.8, and trace amounts of other elements (&lt;0.1). The La2O3 content in the charge varied between 0, 2 and 5 vol. %. The powders were mixed in a planetary mill with ethyl alcohol as the medium for 2 h, using a grinding media to powder ratio of 3:1. Consolidation of the powders was achieved through spark plasma sintering at 1700 °С, applying a pressing pressure of 30 MPa. The heating rate was 50 °С/min, and the isothermal holding time was 5 min. Oxidation was carried out in air at 1200 °С and the total oxidation time was 20 h. Oxidation experiments were conducted in air at 1200 °С, with a total oxidation time of 20 h. It was observed that the most significant weight gain occurred within the first 2–4 h of testing. Specimens containing 5 vol. % La2O3 exhibited the smallest weight gain after 20 h of exposure. Regardless of the presence of La2O3 , silicon carbide was found to be the first material to undergo oxidation. In specimens without La2O3 addition, the oxidized layer mainly consisted of silicon monoxide and dioxide. In contrast, specimens with La2O3 exhibited a predominantly oxidized layer composed of ZrSiO4 and ZrO2 . The study revealed that the introduction of La2O3 intensified the formation of zircon, which subsequently slowed down the oxidation processes in the material.</p></abstract><trans-abstract xml:lang="ru"><p>Исследовано влияние добавки La2O3 на окисление керамики состава, об. %: 80ZrB2–20SiC. В качестве исходных материалов использовали диборид циркония (ООО ДПТП «Вега», Россия), карбид кремния марки 63С (ОАО «Волжский абразивный завод», Россия) и концентрат гидроксида лантана (ОАО «Соликамский магниевый завод», Россия), содержание элементов в котором составляло, мас. %: La – 54,2, Nd – 4,3, Pr – 2,8, остальные – менее 0,1. Содержание La2O3­ в шихте варьировалось: 0, 2 и 5 об. %. Смешивание порошков проводили с использованием планетарной мельницы в течение 2 ч в этиловом спирте, соотношение мелющих тел и порошка составляло 3:1. Консолидацию порошков осуществляли методом искрового плазменного спекания при температуре 1700 °С и давлении прессования 30 МПа со скоростью нагрева 50 °С/мин и изотермической выдержкой 5 мин. Окисление проводили на воздухе при температуре 1200 °С, общее время окисления составило 20 ч. Наиболее интенсивное увеличение массы отмечено в течение первых 2–4 ч испытаний. По истечении 20 ч наименьшее увеличение массы наблюдалось у образцов с добавкой 5 об. % La2O3 . Установлено, что вне зависимости от наличия La2O3 карбид кремния первым подвергается окислению. В образцах без добавки La2O3 окисленный слой состоит преимущественно из моно- и диоксида кремния, тогда как в образцах с La2O3 большую часть окисленного слоя составляют ZrSiO4 и ZrO2 . Таким образом, установлено, что введение La2O3 интенсифицирует процесс формирования циркона, что способствует замедлению процессов окисления.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>окисление</kwd><kwd>искровое плазменное спекание</kwd><kwd>диборид циркония</kwd><kwd>карбид кремния</kwd><kwd>оксид лантана</kwd><kwd>окисленный слой</kwd><kwd>энергодисперсионный анализ</kwd><kwd>элементный состав</kwd></kwd-group><kwd-group xml:lang="en"><kwd>oxidation</kwd><kwd>spark plasma sintering</kwd><kwd>zirconium diboride</kwd><kwd>silicon carbide</kwd><kwd>lanthanum oxide</kwd><kwd>oxidized layer</kwd><kwd>energy dispersive analysis</kwd><kwd>elemental composition</kwd></kwd-group></article-meta></front><body><p>Introduction</p><p>To date, the primary concern lies in the development of materials capable of enduring extended periods in oxidizing environments at high temperatures [1–3]. In this regard, a noteworthy focus is on ultra-high-temperature ceramics (UHTC), which consist of a ceramic matrix and a protective structure that shields the surface from oxidation [1; 4; 5]. In order to produce such materials a deliberate selection of additive phases is conducted to facilitate the formation of surface structures that can withstand prolonged exposure to oxidizing environments at high temperatures. One prevalent example of UHTCs is composite materials based on zirconium or hafnium borides, which exhibit high thermal conductivity and thermal shock resistance [<xref ref-type="bibr" rid="cit6">6</xref>].</p><p>Sintering zirconium and hafnium boride powders requires temperatures exceeding 1950 °C due to their strong covalent bonds and low self-diffusion coefficient [7; 8]. The sintering process is typically activated by incorporating sintering additives such as SiC, Si3N4 , La2O3 , LaB6 [9; 10], tantalum, titanium, zirconium, molybdenum silicides, etc. The optimum composition is considered to be the volumetric ratio of 80 % ZrB2 to 20 % SiC [11; 12]. At high temperatures, the oxidation of these ceramics leads to the formation of a protective multi-layer coating on the surface, consisting of ZrO2–SiO2 and borosilicate glass. This coating effectively seals cracks and pores on the UHTC surface, creating a gas-tight film that prevents oxygen diffusion into the material [13; 14].</p><p>Spark plasma sintering (SPS) is a relatively recent technique that enables the reduction of sintering temperature and time for certain materials when performed under vacuum or an argon atmosphere [<xref ref-type="bibr" rid="cit15">15</xref>]. Despite some existing studies in this area, the phase composition, structure, and oxidation properties of boride-based composite materials produced through this process have not been adequately investigated [15–17].</p><p>The objective of this study was to examine the impact of La2O3 addition on the oxidation properties of composite ceramics with the following volumetric composition: 80ZrB2–20SiC.</p><p> </p><p>Materials and Methods of Research</p><p>The source materials utilized in this study included:</p><p>– zirconium diboride (DPTP Vega LLC., Russia); </p><p>– lanthanum hydroxide concentrate (Solikamsk Magnesium Plant JSC, Russia), with the following elemental content (wt. %): La – 54,2, Nd – 4,3, Pr – 2,8 and trace amounts of other elements (&lt;0.1); </p><p>– grade 63C silicon carbide (Volzhsky Abrasive Works JSC, Russia). </p><p>The particle size distribution of the powders was determined using laser light diffraction with the Analysette 22 NanoTec plant (Fritsch GmbH, Germany). The ZrB2 powder exhibited a predominant particle size range of 0.5 to 12 μm, with 97 % of particles measuring less than 11.1 μm, and an average particle size of 4.52 μm. The SiC powder demonstrated a bimodal particle size distribution, with an average particle size of 3.47 μm. The La(OH)3 powder exhibited a wide particle size distribution, with an average particle size of 9.76 μm.</p><p>In order to convert lanthanum hydroxide into oxide, the material was subjected to annealing at 600 °C for a duration of 1 h in an air atmosphere. The initial powders were mixed using a SAND planetary mill in ethyl alcohol. The grinding process lasted for 2 h at a speed of 160 rpm, a grinding media to powder ratio of 3:1. The mixtures contained lanthanum oxide in two different volumetric percentages: 0, 2 and 5.</p><p>The specimens were consolidated using spark plasma sintering (SPS) on the Dr. Synter SPS-1050b equipment (SPS Syntex, Japan) at a temperature of 1700 °C. Heating was achieved by applying a pulsed direct current at a rate of 50 °C per min. The temperature was monitored using an optical pyrometer placed on the outer side of the graphite matrix. The material was loaded into the system just before the heating process began, while maintaining a constant load at a pressure of 30 MPa. The applied load was removed after the completion of the heating phase. To prevent any undesirable reactions between the sintered powder, matrix, and punches, graphite paper was employed. Additionally, graphite felt was wrapped around the mold to minimize heat losses. The specimens were subjected to an isothermal holding time of 5 min. </p><p>The apparent density and open porosity of sintered specimens were analyzed following the guidelines outlined in GOST 2409-2014. </p><p>For the oxidation study, the specimens were exposed to air in an electric furnace equipped with silicon carbide heaters. The crucibles containing the specimens were placed in the furnace, preheated to 1200 °C. After a specific duration, the specimens were removed, weighed to record their weight, and then returned to the furnace. The total duration of high-temperature oxidation was 20 h.</p><p>The phase composition of the specimens was examined using Raman spectroscopy on a multifunction spectrometer SENTERRA (Bruker, Germany), with a laser wavelength of 532 nm. The acquired data were processed using the OPUS 6.5 software.</p><p>Microscopic analysis of the specimens was conducted using an analytical auto emission scanning electron microscope VEGA3 (TESCAN, Czech Republic). In order to determine the elemental composition, an Inca X-Act detector (Oxford Instruments Analytical, Great Britain) was employed for energy-dispersive analysis of the elemental composition of the materials.</p><p> </p><p>Results and Discussion</p><p>The investigations were conducted on the materials containing 0, 2 and 5 vol. % of La2O3 . No significant changes in the apparent density and open porosity of the specimens were observed after the SPS process. The open porosity values ranged from 3.5 to 5.5 % across all variations. </p><p>The specimens were subjected to oxidation in an air environment for a duration of 20 h. The time intervals for recording the specific weight gain of the specimens increased as the weight gain decreased. The results are presented in Figure 1. The most substantial weight gain occurred within the initial 2–4 h of testing. </p><p> </p><p> </p><p>Among the specimens, those with 5 vol. %. of La2O3 exhibited the lowest weight gain after the 20-hour exposure. It is worth noting that up to 9 h of exposure, the differences in specific weight gain were minimal. Only with further increases in oxidation time did the impact of La2O3 on the material’s oxidation resistance become more pronounced.</p><p>It has been established that the resistance of ZrB2 composite materials to high-temperature oxidation is primarily influenced by the composition of the protective layer formed on the material’s surface [<xref ref-type="bibr" rid="cit18">18</xref>]. The fractures in the specimens were examined using scanning electron microscopy (SEM) along with energy dispersive analysis. SEM images and maps displaying the distribution of silicon, zirconium, and boron within the specimens were obtained (Figure 2: spectrum 1 represents the surface layer of the specimen; spectrum 2 corresponds to an internal structure displaying significant visual dissimilarity; spectrum 3 pertains to a deeper layer of the material).</p><p> </p><p> </p><p>In the specimen without the addition of La2O3 , a continuous protective layer composed of silicon-containing phases is formed on its surface (spectrum 1 in Fig. 2). When La2O3 is introduced, the silicon content on the specimen surface is also higher (spectrum 1) compared to the subsequent layers (spectra 2 and 3). However, the thickness of these layers is significantly reduced. Figure 3 presents a histogram depicting the calculated thickness of the oxidized layers, determined through analysis of the material’s microstructure (as shown in Figure 2).</p><p> </p><p> </p><p>Table 1 displays the outcomes of the energy dispersive analysis, providing the elemental composition of the specimens following a 20-hour oxidation process. The first layer exhibits identical composition across all three cases. Notably, boron is not detected in the spectra, which is consistent with the challenges in accurately capturing elements from the second period of the periodic table using spectral methods [<xref ref-type="bibr" rid="cit19">19</xref>].</p><p> </p><p> </p><p>Table 2 presents the results of calculating the atomic composition of the layers, with values rounded to the first decimal place after considering the atomic weights of the elements (and then multiplied by 10). </p><p> </p><p> </p><p>The assumed chemical composition is derived from the known composition of the initial specimens and the determined element ratios within the layers. The primary stoichiometric phases that are likely to be present are listed in Table 2. It should be noted that the formation of silicon monoxide as a crystalline compound has been previously documented in multiple instances [20–22]. </p><p>The possibility of non-stoichiometric compound formation, such as borosilicate and borate glasses, should also be taken into consideration [<xref ref-type="bibr" rid="cit23">23</xref>].</p><p>Raman spectroscopy confirmed the presence of zircon (ZrSiO4) and monoclinic zirconium dioxide (ZrO2) as the main phases of the oxidized material (Figure 4) [<xref ref-type="bibr" rid="cit24">24</xref>]. The imaging was conducted from the surface of the specimens, thereby removing the first layer. One of the obtained spectra is presented, with the others being identical. The only distinction lies in the intensity ratio of the peaks corresponding to the main phases. The absence of silicon oxide lines in the specimen without lanthanum addition can be explained by the fact that well-oxidized phases in the second layer hinder the detection of amorphous or concealed-crystalline silicon oxide phases.</p><p>There is a noticeable disparity in the distribution of zirconium on the surface of specimens with and without La2O3 (Figure 5, a–c). In the case without La2O3 , ZrO2 , despite its relatively low overall content (as seen in Table 1), is distributed relatively (Figure 5, a). Presumably, it is integrated within the primary silicon-containing phases. However, the addition of lanthanum oxide results in the growth of zirconium-bearing phase grains and the emergence of agglomerates and large pores between these phases. In this scenario, the formation of silicon oxides is unlikely.</p><p> </p><p> </p><p>Figure 5, d illustrates a fragment of the boron distribution map in the upper layer of the specimen containing 5 vol. % La2O3 , corresponding to the fragment of the zirconium distribution map in Figure 5, c. Since boron could not be detected during the determination of the mass content of elements (as indicated in Table 1), it can be inferred that boron is present in the form of silicate glasses (refer to Figure 2, f ) that fill the gaps between zircon and zirconium dioxide grains [<xref ref-type="bibr" rid="cit25">25</xref>].</p><p>Consequently, on the surface of specimens without La2O3 additives, phases comprising silicon oxides with traces of boron and zirconium oxides are formed. In the presence of La2O3 additives, the main phases observed are zirconium dioxide and zircon, along with an excess of oxygen. However, neither case effectively acts as a significant barrier against the deep penetration of oxygen into the material. The presence of lanthanum oxide appears to enhance the formation of zircon, a phase that exhibits greater resistance to thermal shock than monoclinic zirconium dioxide and contributes to the deceleration of the oxidation process.</p><p> </p><p>Conclusion</p><p>The aim of the study was to investigate the impact of La2O3 addition on the oxidation properties of composite ceramics with a composition of 80 vol. % ZrB2 and 20 vol. % SiC, consolidated through spark plasma sintering. The materials were examined in three variations: without La2O3 , with 2 vol. % La2O3 and 5 vol. % La2O3 . In all cases, SiC acted as a sacrificial material, being the first to undergo oxidation. Specimens without La2O3 addition exhibited a surface layer consisting mainly of SiO2 and SiO. On the other hand, specimens with La2O3 addition showcased surface layers composed primarily of ZrSiO4 and ZrO2 .</p><p>Consequently, the introduction of La2O3 intensified the formation of zircon and decelerated the oxidation processes. However, it did not serve as a complete barrier to the deep penetration of oxygen into the material.</p><p> </p></body><back><ref-list><title>References</title><ref id="cit1"><label>1</label><citation-alternatives><mixed-citation xml:lang="ru">Григорьев О.Н., Фролов Г.А., Евдокименко Ю.И., Кисель В.М., Панасюк А.Д., Мелах Л.М., Котенко В.А., Коротеев А.В. Ультравысокотемпературная керамика для авиационно-космической техники. Авиационно-космическая техника и технология. 2012;8(95):119–128.</mixed-citation><mixed-citation xml:lang="en">Grigor’ev O.N., Frolov G.A., Evdokimenko Ju.I,. Kisel’ V.M., Panasjuk A.D., Melah L.M., Kotenko V.A., Koroteev A.V.Ultra-high temperature ceramics for aerospace technology. Aviacionno-kosmicheskaja tehnika i tehnologija. 2012;8(95):119–128. (In Russ.).</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Наруцкая А.С., Истомин Н.Д. Окислительное поведение высокотемпературных керамик на основе диборида циркония. Перспективы развития фундаментальных наук. В сб.: Труды XVIII Международной конференции студентов, аспирантов и молодых ученых (Томск, 27–30 апреля 2021 г.). Т. 2. Химия. Под ред. И.А. Курзиной, Г.А. Вороновой. Томск: Изд-во Томского политехнического университета, 2021. C. 164–166.</mixed-citation><mixed-citation xml:lang="en">Naruckaja A.S., Istomin N.D. Oxidative behavior of high-temperature ceramics based on zirconium diboride. Prospects for the Development of Fundamental Sciences. In: Proceedings of the XVIII International Conference of Students, Postgraduates and Young Scientists (Tomsk, 27–30.04.2021). Vol. 2. Khimija (Eds. I.A. Kurzina, G.A. Voronova. Tomsk: Tomskii politehnicheskii universitet, 2021. P. 164–166. (In Russ.).</mixed-citation></citation-alternatives></ref><ref id="cit3"><label>3</label><citation-alternatives><mixed-citation xml:lang="ru">Яцюк И.В., Потанин А.Ю. Рупасов С.И., Левашов Е.А. Кинетика и механизм высокотемпературного окисления керамических материалов в системе ZrB2–SiC–MoSi2. Известия вузов. Цветная металлургия. 2017;(6):63–69. https://doi.org/10.17073/0021-3438-2017-6-63-69</mixed-citation><mixed-citation xml:lang="en">Iatsyuk I.V., Potanin A.Yu., Rupasov S.I., Levashov E.A. Kinetics and high-temperature oxidation mechanism of ceramic materials in ZrB2–SiC–MoSi2 system. Russian Journal of Non-Ferrous Metals. 2018;59(1):76–81. https://doi.org/10.3103/S1067821218010157</mixed-citation></citation-alternatives></ref><ref id="cit4"><label>4</label><citation-alternatives><mixed-citation xml:lang="ru">Житнюк С.В. Бескислородные керамические материалы для аэрокосмической техники (обзор). Труды ВИАМ. 2018;(8):81–88. https://doi.org/10.18577/2307-6046-2018-0-8-81-88</mixed-citation><mixed-citation xml:lang="en">Zhitnyuk S.V. Oxygen-free ceramic materials for the space technics (review). Trudy VIAM. 2018;(8):81–88. (In Russ.). https://doi.org/10.18577/2307-6046-2018-0-8-81-88</mixed-citation></citation-alternatives></ref><ref id="cit5"><label>5</label><citation-alternatives><mixed-citation xml:lang="ru">Пойлов В.З., Прямилова Е.Н. Термодинамика окисления боридов циркония и гафния. Журнал неорганичес­кой химии. 2016;61(1):59–62. https://doi.org/10.7868/S0044457X16010190</mixed-citation><mixed-citation xml:lang="en">Poilov V.Z., Pryamilova E.N. Thermodynamics of oxidation of zirconium and hafnium borides. Russian Journal of Inorganic Chemistry. 2016;61(1):55–58. https://doi.org/10.1134/S0036023616010198</mixed-citation></citation-alternatives></ref><ref id="cit6"><label>6</label><citation-alternatives><mixed-citation xml:lang="ru">Li W., Cheng T., Li D., Fang D. Numerical simulation for thermal shock resistance of ultra high temperature cera­mics considering the effects of initial stress field. Advances in Materials Science and Engineering. 2011;1–7:757543. https://doi.org/10.1155/2011/757543</mixed-citation><mixed-citation xml:lang="en">Li W., Cheng T., Li D., Fang D. Numerical simulation for thermal shock resistance of ultra high temperature cera­mics considering the effects of initial stress field. Advances in Materials Science and Engineering. 2011;1–7:757543. https://doi.org/10.1155/2011/757543</mixed-citation></citation-alternatives></ref><ref id="cit7"><label>7</label><citation-alternatives><mixed-citation xml:lang="ru">Rangaray L., Surecha S.J, Divakar C., Jayaram V. Low-temperature processing of ZrB2–ZrC composites by reactive hot pressing. Metallurgical and Materials Transactions A. 2008;39(7):1496–1505. https://doi.org/10.1007/s11661-008-9500-y</mixed-citation><mixed-citation xml:lang="en">Rangaray L., Surecha S.J, Divakar C., Jayaram V. Low-temperature processing of ZrB2–ZrC composites by reactive hot pressing. Metallurgical and Materials Transactions A. 2008;39(7):1496–1505. https://doi.org/10.1007/s11661-008-9500-y</mixed-citation></citation-alternatives></ref><ref id="cit8"><label>8</label><citation-alternatives><mixed-citation xml:lang="ru">Gasch M.J., Ellerby D.T., Johnson S.M. Ultra high temperature ceramic composites. In: Handbook of Ceramic Composites. Springer, Boston. MA, 2005. P. 197–224. https://doi.org/10.1007/0-387-23986-3_9</mixed-citation><mixed-citation xml:lang="en">Gasch M.J., Ellerby D.T., Johnson S.M. Ultra high temperature ceramic composites. In: Handbook of Ceramic Composites. Boston: Springer,  2005. P. 197–224. https://doi.org/10.1007/0-387-23986-3_9</mixed-citation></citation-alternatives></ref><ref id="cit9"><label>9</label><citation-alternatives><mixed-citation xml:lang="ru">Gozalez-Julian J., Cedillos-Barraza O., Döringet S. Enhanced oxidation resistance of ZrB2/SiC composite through in situ reaction of gadolinium oxide in patterned surface cavities. Journal of the European Ceramic So­ciety. 2014;34(16):4157–4166. https://doi.org/10.1016/j.jeurceramsoc.2014.07.015</mixed-citation><mixed-citation xml:lang="en">Gozalez-Julian J., Cedillos-Barraza O., Döringet S. Enhanced oxidation resistance of ZrB2/SiC composite through in situ reaction of gadolinium oxide in patterned surface cavities. Journal of the European Ceramic So­ciety. 2014;34(16):4157–4166. https://doi.org/10.1016/j.jeurceramsoc.2014.07.015</mixed-citation></citation-alternatives></ref><ref id="cit10"><label>10</label><citation-alternatives><mixed-citation xml:lang="ru">Paul A., Jayaseelan D.D., Venugopal S., Zapata-Sol­vas E., Binner J., Vaidhyanathan B., Heaton A., Brown P., Lee W.E. UHTC composites for hypersonic applications. American Ceramic Society Bulletin. 2012; 91(1);22–29.</mixed-citation><mixed-citation xml:lang="en">Paul A., Jayaseelan D.D., Venugopal S., Zapata-Sol­vas E., Binner J., Vaidhyanathan B., Heaton A., Brown P., Lee W.E. UHTC composites for hypersonic applications. American Ceramic Society Bulletin. 2012; 91(1);22–29.</mixed-citation></citation-alternatives></ref><ref id="cit11"><label>11</label><citation-alternatives><mixed-citation xml:lang="ru">Chamberlain A., Fahrenholtz W., Hilmas G., Ellerby D. Oxidation of ZrB2–SiC ceramics under atmospheric and reentry conditions. Refractory Applications Transactions. 2005;1(2):1–8.</mixed-citation><mixed-citation xml:lang="en">Chamberlain A., Fahrenholtz W., Hilmas G., Ellerby D. Oxidation of ZrB2–SiC ceramics under atmospheric and reentry conditions. Refractory Applications Transactions. 2005;1(2):1–8.</mixed-citation></citation-alternatives></ref><ref id="cit12"><label>12</label><citation-alternatives><mixed-citation xml:lang="ru">Bellosi A., Monteverde F. Fabrication and properties of zirconium diboride-based ceramics for UHT applications. In: Proc. 4th European Workshop. «Hot Structures and Thermal Protection Systems for Space Vehicles» (Palermo, Italy 26–29 November 2002). Paris: European Space Agency, 2003. P. 65–71.</mixed-citation><mixed-citation xml:lang="en">Bellosi A., Monteverde F. Fabrication and properties of zirconium diboride-based ceramics for UHT applications. In: Proc. 4th European Workshop. «Hot Structures and Thermal Protection Systems for Space Vehicles» (Palermo, Italy 26–29 November 2002). Paris: European Space Agency, 2003. P. 65–71.</mixed-citation></citation-alternatives></ref><ref id="cit13"><label>13</label><citation-alternatives><mixed-citation xml:lang="ru">Justin J.F., Jankowiak A. Ultra high temperature cera­mics: densification, properties and thermal stability. AerospaceLab Journal. 2011;3:1–11.</mixed-citation><mixed-citation xml:lang="en">Justin J.F., Jankowiak A. Ultra high temperature cera­mics: densification, properties and thermal stability. AerospaceLab Journal. 2011;3:1–11.</mixed-citation></citation-alternatives></ref><ref id="cit14"><label>14</label><citation-alternatives><mixed-citation xml:lang="ru">Bellosi A., Guicciardi S., Medri V., Monteverde F., Scitti D., Silvestroni L. Processing and properties of ultra-refractory composites based on Zr- and Hf-borides: state of the art and perspectives. In: Boron rich solids: Sensors, ultra high temperature ceramics, thermoelectrics, armor. 2011, P.147–160. https://doi.org/10.1007/978-90-481-9818-4</mixed-citation><mixed-citation xml:lang="en">Bellosi A., Guicciardi S., Medri V., Monteverde F., Scitti D., Silvestroni L. Processing and properties of ultra-refractory composites based on Zr- and Hf-borides: state of the art and perspectives. In: Boron rich solids: Sensors, ultra high temperature ceramics, thermoelectrics, armor. 2011, P. 147–160. https://doi.org/10.1007/978-90-481-9818-4</mixed-citation></citation-alternatives></ref><ref id="cit15"><label>15</label><citation-alternatives><mixed-citation xml:lang="ru">Sonber J. K., Suri A. K. Synthesis and consolidation of zirconium diboride: review. Advanced in applied ceramics. Structural, Functional and Bioceramics. 2011;110(6): 321–334. https://doi.org/10.1179/1743676111Y.0000000008</mixed-citation><mixed-citation xml:lang="en">Sonber J. K., Suri A. K. Synthesis and consolidation of zirconium diboride: review. Advanced in applied cera­mics. Structural, Functional and Bioceramics. 2011;110(6):321–334. https://doi.org/10.1179/1743676111Y.0000000008</mixed-citation></citation-alternatives></ref><ref id="cit16"><label>16</label><citation-alternatives><mixed-citation xml:lang="ru">Sciti D., Silvestroni L., Bellosi A. Fabrication and properties of HfB2–MoSi2 composites produced by hot pressing and spark plasma sintering. Journal of Materials Science. 2006;21(6):1460–1466. https://doi.org/10.1557/jmr.2006.0180</mixed-citation><mixed-citation xml:lang="en">Sciti D., Silvestroni L., Bellosi A. Fabrication and properties of HfB2–MoSi2 composites produced by hot pressing and spark plasma sintering. Journal of Materials Science. 2006;21(6):1460–1466. https://doi.org/10.1557/jmr.2006.0180</mixed-citation></citation-alternatives></ref><ref id="cit17"><label>17</label><citation-alternatives><mixed-citation xml:lang="ru">Перевислов С.Н., Несмелов Д.Д., Томкович М.В. Получение материалов на основе SiCi и Si3N4 методом высокотемпературного плазменного спекания. Физика твердого тела. Вестник Нижегородского университета им. Н.И. Лобачевского. 2013;2(2):107–114.</mixed-citation><mixed-citation xml:lang="en">Perevislov S.N., Nesmelov D.D., Tomkovich M.V.  SiC and Si3N4-based materials obtained by spark plasma sintering. Fizika tverdogo tela. Vestnik Nizhegorodskogo universiteta imeni N.I. Lobachevskogo. 2013;2(2):107–114. (In Russ.).</mixed-citation></citation-alternatives></ref><ref id="cit18"><label>18</label><citation-alternatives><mixed-citation xml:lang="ru">Hurbert D.M., Jiang D., Dudina D.V., Mukherjee A.K. The synthesis and consolidation of hard materials by spark plasma sintering. International Journal of Refractory Metals and Hard Materials. 2009;27(2):367–375. https://doi.org/10.1016/j.ijrmhm.2008.09.011</mixed-citation><mixed-citation xml:lang="en">Hurbert D.M., Jiang D., Dudina D.V., Mukherjee A.K. The synthesis and consolidation of hard materials by spark plasma sintering. International Journal of Refractory Metals and Hard Materials. 2009;27(2):367–375. https://doi.org/10.1016/j.ijrmhm.2008.09.011</mixed-citation></citation-alternatives></ref><ref id="cit19"><label>19</label><citation-alternatives><mixed-citation xml:lang="ru">Хиллер В.В. Рентгеноспектральный микроанализ содержания бора в сердцевине заготовок оптоволокна. Проблемы теоретической и экспериментальной химии. В сб.: Тезисы докладов XXIV Российской молодежной научной конференции, посвященной 170-летию открытия химического элемента рутений (Екатеринбург, 23–25 апреля 2014 г.). Екатеринбург: Изд-во УрФУ, 2014. C. 80–81.</mixed-citation><mixed-citation xml:lang="en">Hiller V.V. X-ray spectral microanalysis of boron content in the core of fiber blanks. problems of theoretical and experimental chemistry. In: Abstracts of the XXIV Russian Youth Scientific Conference Dedicated to the 170th Anniversary of the Discovery of the Chemical Element Ruthenium (Ekaterinburg, 23–25.04.2014). Yekaterinburg: Izdatel’stvo UrFU, 2014. P. 80–81. (In Russ.).</mixed-citation></citation-alternatives></ref><ref id="cit20"><label>20</label><citation-alternatives><mixed-citation xml:lang="ru">Грибов Б.Г., Зиновьев К.В., Калашник О.Н., Герасименко Н.Н., Смирнов Д.И., Суханов В.Н. Структура и фазовый состав монооксида кремния. Известия вузов. Электроника. 2011;4(90);3–8.</mixed-citation><mixed-citation xml:lang="en">Gribov B.G., Zinov’ev K.V., Kalashnik O.N., Gerasimenko N.N., Smirnov D.I., Sukhanov V.N. Structure and phase composition of silicon monoxide. Semiconductors. 2012;46(13):1576–1579. https://doi.org/10.1134/S106378261213009X</mixed-citation></citation-alternatives></ref><ref id="cit21"><label>21</label><citation-alternatives><mixed-citation xml:lang="ru">Al Kaabi Khalid, Prasad Dasari L.V.K., Kroll P. Silicon monoxide at 1 atm and elevated pressures: Crystalline or Amorphous? Journal of the American Chemical Society. 2014;136(9):3410–3423. https://doi.org/10.1021/ja409692c</mixed-citation><mixed-citation xml:lang="en">Al Kaabi Khalid, Prasad Dasari L.V.K., Kroll P. Silicon monoxide at 1 atm and elevated pressures: Crystalline or Amorphous? Journal of the American Chemical Society. 2014;136(9):3410–3423. https://doi.org/10.1021/ja409692c</mixed-citation></citation-alternatives></ref><ref id="cit22"><label>22</label><citation-alternatives><mixed-citation xml:lang="ru">Грибов Б.Г., Зиновьев К.В., Калашник О.Н., Герасименко Н.Н., Смирнов Д.И., Суханов В.Н. Выращивание нанокристаллического кремния из матрицы аморфного монооксида кремния. Известия вузов. Электроника. 2012;96(4):13–18.</mixed-citation><mixed-citation xml:lang="en">Gribov B.G., Zinov’ev K.V., Kalashnik O.N., Gerasimenko N.N., Smirnov D.I., Sukhanov V.N. Growth of nanocrystalline silicon from a matrix of amorphous silicon monoxide. Semiconductors. 2013;47(13):1684–1686. https://doi.org/10.1134/S1063782613130071</mixed-citation></citation-alternatives></ref><ref id="cit23"><label>23</label><citation-alternatives><mixed-citation xml:lang="ru">Ehrt D. Structure, properties and applications of borate glasses. Glass Technology: European Journal of Glass Science and Technology. Part A. 2000;41(6):182–185.</mixed-citation><mixed-citation xml:lang="en">Ehrt D. Structure, properties and applications of borate glasses. Glass Technology: European Journal of Glass Science and Technology. Part A. 2000;41(6):182–185.</mixed-citation></citation-alternatives></ref><ref id="cit24"><label>24</label><citation-alternatives><mixed-citation xml:lang="ru">Орлов Р.Ю., Вигасина М.Ф., Успенская М.Е. Спектры комбинационного рассеяния минералов: Справочник. М.: ГЕОС, 2007. 142 с.</mixed-citation><mixed-citation xml:lang="en">Orlov R.Yu., Vigasina M.F., Uspenskaya M.E. Raman spectra of minerals (reference book). Moscow: GEOS, 2007. 142 p. (In Russ.).</mixed-citation></citation-alternatives></ref><ref id="cit25"><label>25</label><citation-alternatives><mixed-citation xml:lang="ru">Баньковская И.Б., Коловертнов Д.В. Влияние режима термообработки на состав и структуру композитов системы ZrB2–SiC. Физика и химия стекла. 2013;39(5):816–828.</mixed-citation><mixed-citation xml:lang="en">Ban’kovskaya I.B., Kolovertnov D.V. Effect of the thermal treatment mode on the composition and structure of ZrB2–SiC system composites. Glass Physics and Che­mistry. 2013;39(5);579–588. https://doi.org/10.1134/S1087659613050027</mixed-citation></citation-alternatives></ref></ref-list><fn-group><fn fn-type="conflict"><p>The authors declare that there are no conflicts of interest present.</p></fn></fn-group></back></article>
