Vacuum arc coatings for combastion chambers of rocket engines

1Nadtoka, VM, 1Husarova, IA, 1Kraiev, MV, 2Borysenko, АY, 1Bondar, DM, 1Osinovyj, GG
1Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
2Z. I. Nekrasov Iron and Steel Institute of the National Academy of Science of Ukraine, Dnipro, Ukraine
Space Sci. & Technol. 2024, 30 ;(5):19-28
https://doi.org/10.15407/knit2024.05.019
Мова публікації: English
Анотація: 
An investigation was done for heat-resistant coatings from Ni-Cr and Fe-Ni-Cr alloys, produced by vacuum arc deposition with cathodes from nichrome alloy ХН78Т and steel 12Х18Н10Т. The microstructural analysis of the studied coatings applied by vacuum arc deposition with different amounts of reactive gas (nitrogen) in a deposition chamber showed the presence of two phases: a matrix and the distributed particles of liquid phase of various sizes and shapes. Vacuum arc deposition at a cathode arc current of 55 A for Ni-Cr and 82 A for Fe-Ni-Cr coatings, a cathode arc voltage of 28 to 32 V, an underlayer temperature of 490±30 оС, and no nitrogen in the chamber gives coatings with no apparent orientation of crystallites and a microhardness reaching 330 to 374 HV. The diffusion mobility of atoms decreases at a higher nitrogen pressure, which results in a coarse-crystal, porous-columnar structure of coatings with high porosity, a varying volume, and a rough surface. The influence of nitrogen pressure in a chamber on the strength of coatings was evaluated by their microhardness. A nitrogen pressure gain up to 0.13 Pa results in the increased microhardness of both coating
systems, and the further growth in pressure has almost no effect on microhardness. It was discovered that a nitrogen pressure of 0.13 Pa gives the optimum combination of a coating’s strength and continuous structure with no pores and apparent columnar crystallites Alloys from Ni-Cr with 80 % Ni are among the most heat-resistant industrial materials with a maximum operating temperature of up to 1200 оС. However, they are expensive, which makes Fe-Ni-Cr alloys more attractive, providing their heat resistance is sufficient for the operating temperature range. Therefore, it is reasonable to conduct further research on both Ni-Cr and Fe-Ni-Cr coatings to develop a deposition technology that can provide the required performance parameters. Controlling nitrogen pressure makes it possible to adjust the structure and properties of the coating during deposition.
Ключові слова: Fe-Ni-Cr heat-resistant coatings, microhardness, microstructure, Ni-Cr
References: 
1. Andreev A. A. (2009). Physico-technological foundations of vacuum-arc hardening of surfaces: abstract for the scientific degree of Doctor of Technical Sciences. Kharkiv: IERT NAS of Ukraine, 28 p. [In Russian].
2. Andreev A. A., Sablev L. P., Grigoriev S. N. (2010). Vacuum arc coatings. Kharkiv: NSC “KIPT”, 318 p. [In Russian].
3. Andreev A. A., Sablev L. P., Shulaev V. M., Grigoriev S. N. (2005). Vacuum-arc devices and coatings. Kharkiv: NSC “KIPT” 236 p. [In Russian].
4. Azarenkov N. A., Sobol O. V., Pogrebnyak A. D., Beresnev V. M. (2011). Engineering of vacuum-plasma coatings: monograph. Kharkiv: KhNU named after V. N. Karazin, 343 p. [In Russian].
5. Bilyk I. I., Rudenkyi S. O. (2023). The technology of applying coatings and their power. Kyiv: KPI named after Igor Sikorsky, art. 50. [In Ukrainian].
6. Eremin E. N., Yurov V. M., Laurynas V. Ch., Syzdykova A. Sh. (2019). The influence of technological parameters for applying multi-element ion plasma coatings on their quality. Omsk scientific journal. Mechanical Engineering and Mechanical science, No 4 (166), 9-13 [In Russian].
7. Fiedler T., Fedorova T., Rösler J., Bäker M. (2014). Design of a Nickel-Based Bond-Coat Alloy for Thermal Barrier Coatings on Copper Substrates. Metals, 4(4), 503-518.
https://doi.org/10.3390/met4040503
8. Gahun G. G., Baulin V. I., Volodin V. A., Kurpatenkov V. D. (1989). Construction and design of liquid-propellant rocket engines. M.: Mechanical Engineering, 420 p. [In Russian].
9. Goldshtein M. I., Grachev S. V., Veksler Yu. G. (1985). Special steels. Textbook for universities. M.: Metallurgy, 408 p. [In Russian].
10. Golizadeh M., Mendez M. F., Kolozsvári S., Anders A., Franz R. (2021). Cathode spot behavior in nitrogen and oxygen gaseous atmospheres and concomitant cathode surface modifications. Surface & Coatings Technology, 421.
https://doi.org/10.1016/j.surfcoat.2021.127441.
11. GOST 5632-72 “High-alloy steels and corrosion-resistant, heat-resistant and heat-resistant alloys. Steel grades”
12. Hasii O. B. (2018). Development of technology for vacuum ion-plasma filing and direct improvement. Sci. bull. NLTU of Ukraine, 28, № 10 [In Ukrainian].
13. Karimi Aghda S., Music D., Unutulmazsoy Y., Sua H. H., Mráz S., Hans M., Primetzhofer D., Anders A., Schneider J. M. (2021). Unraveling the ion-energy-dependent structure evolution and its implications for the elastic properties of (V, Al)N thin films. Acta Materialia, 214(3), 117003.
https://doi.org/10.1016/j.actamat.2021.117003.
14. Khoroshikh V. M. (2004). Droplet phase of cathode erosion of a stationary vacuum arc. Phys. surface engineering, 2, No 4, 200-213 [In Russian].
15. Lewis J. R. (1975). Materials and Processes for Space Shuttle’s Engines. Metal Progress, American Society for Materials.
16. Liquid rocket engines.
URL: http://www.lpre.de/index.htm (Last accessed 09/07/2023).
17. Movchan B. A., Malashenko I. S. (1983). Heat-resistant coatings deposited in vacuum. K.: Naukova Dumka, 232 p. [In Russian].
18. Ogbuji L. (2005). A tabletop technique for assessing the blanching resistance of Cu alloys. Oxidation of Metals, 63(5), 383-399.
https://doi.org/10.1007/s11085-005-4393-2.
19. Riccius J., Haidn O., Zametaev E. (2004). Influence of Time-Dependent Effects on the Estimated Life Time of Liquid Rocket Combustion Chamber Walls. Proc. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit; AIAA: Fort Lauderdale, FL, USA.
20. Rocketdyne F-1 Manuals.
URL: https://archive.org/details/rocketdyne-f-1-manuals (Last accessed: 06.09.24).
21. Schloesser J., Kowollik D., Bäker M., Rösler J., Horst P. (2011). Thermal Barrier Coatings in Rocket Engines-A Multiscale Simulation and Development Approach. Sonderforschungsbereich / Transregio 40-Annual Report 2011; SFB/TRR 40: Garching, Germany, 207-219.
22. Simpson M. A., Smith T. F. (1982). Aust. J. Phys., 35, 307—319. Phase Diagrams of Binary Nickel Alloys, 1991. Complete evaluation contains 4 figures, 4 tables, and 128 references.
23. Sorokin V. G., Volosnikova A. V., Viatkin S. A., et al. (1989). Brand of steels and alloys. M.: Mechanical Engineering, 640 p. [In Russian].