Abstract and keywords
Abstract (English):
The most thermally loaded structural elements of liquid rocket engines, features of their work and protection against thermal effects, as well as the technological process of processing of the transition sections of heat-protective coating of cermets, the influence of quality of treatment on resistance to the formation of defects in bench firing tests of the combustion chamber as part of the engine

Keywords:
cooling, combustion chamber, coating, cermet, processing, abrasive, defect
References

1. Naukoemkie tehnologii v mashinostroenii / Pod red. A.G. Suslova. M.: Mashinostroenie, 2012. 528 s.

2. Spravochnik tehnologa / Pod redakciey A. G. Suslova / M.: Innovacionnoe mashinostroenie, 2019. 800 s.

3. Organizacionnye i ekonomicheskie issledovaniya v mashinostroenii / Pod red. V. P. Smolenceva. Voronezh: VGTU, 2006. 73 s.

4. Safonov S. V. Tehnologicheskoe obespechenie ekspluatacionnyh harakteristik izdeliy. Voronezh: IPC VGU, 2015. 224 s.

5. Smolencev V. P. Proektirovanie tehnologicheskih processov polucheniya vysokoresursnyh kombinirovannyh pokrytiy / V. P. Smolencev, M. V. Kondrat'ev. V. V. Ivanov / Uprochnyayuschie tehnologii i pokrytiya, 2017, № 6-S.273-281

6. Samsonov G. V. Tugoplavkie pokrytiya / G. V., Samsonov, A. P Epik / M.: Metallurgiya, 1973. 398 s.

7. Baldaev L. H. Geotermicheskoe napylenie. M.: Market DS, 2007. 344 s.

8. Hasuy A. Tehnika napyleniya. M.: Mashinostroenie, 1975. 288 s.

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