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Nanoscience and Technology: An International Journal

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ISSN Print: 2572-4258

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The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 1.3 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 1.7 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.7 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00023 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.11 SJR: 0.244 SNIP: 0.521 CiteScore™:: 3.6 H-Index: 14

Indexed in

HEAT-RESISTANT NON-FIRED REPAIR COATINGS FOR PROTECTION OF CARBON-BASE MATERIALS

Volume 5, Issue 4, 2014, pp. 267-285
DOI: 10.1615/NanomechanicsSciTechnolIntJ.v5.i4.20
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ABSTRACT

The method for generating heat-resistant protective coatings of silicide type by non-fired technology is presented. The binder of the slip suspension was a nanodispersed silica sol, and the fillers were powders of the previously developed materials of the Si−TiSi2−MoSi2−B−Y and Si−TiSi2−MoSi2−B−Y−SiC systems. Such coatings are designed to protect heat-resistant carbon-base materials (carbon−carbon composite materials (CCCM) and carbon−ceramic matrix composites (CCMC), structural graphite) against high-temperature gas corrosion. This method allows one to minimize the problems encountered when it is necessary to protect the connecting units of the prefabricated structural elements, inter alia, elements of high dimensions (wing edges, protective screens, casings, etc.), as well as to solve problems related to repair of various damages of standard coatings that are inevitable during the assembly and/or operation of the space-rocket hardware.

CITED BY
  1. Astapov Alexey N., Rabinskiy Lev N., Investigation of Destruction Mechanisms for Heat-Resistant Coatings in Hypersonic Flows of Air Plasma, Solid State Phenomena, 269, 2017. Crossref

  2. Astapov Alexey N., Zhestkov Boris E., Lifanov Ivan P., Rabinskiy Lev N., Terentieva Valentina S., Erosion-Resistant Enhancement of Anti-oxidation Coatings in Hypersonic Flows of Air Plasma, Arabian Journal for Science and Engineering, 44, 6, 2019. Crossref

  3. Astapov A. N., Lifanov I. P., Prokofiev M. V., High-Temperature Interaction in the ZrSi2–ZrSiO4 System and Its Mechanism, Russian Metallurgy (Metally), 2019, 6, 2019. Crossref

  4. Astapov A. N., Zhavoronok S. I., Kurbatov A. S., Rabinskiy L. N., Tushavina O. V., Main Problems in the Creation of Thermal-Protection Systems Based on Structurally Heterogeneous Materials and the Methods of Their Solution, High Temperature, 59, 2-6, 2021. Crossref

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