Additive technologies in the creation of rocket engines with variable specific impulse: modern approaches and perspectives
DOI:
https://doi.org/10.34185/1562-9945-2-163-2026-08Keywords:
additive manufacturing, 3D printing, SLM, DED EBM, topological optimization, functional gradient materials, cooling channels, modular nozzlesAbstract
The article examines the prospects of using additive technologies (3D printing) in the design and manufacture of rocket engines with variable specific impulse, which is one of the priority areas of development in the modern rocket and space industry. The relevance of the study is determined by the need to increase the efficiency, adaptability and reliability of power plants in conditions of variable thermogasdynamic and mechanical loads. The purpose of the work is to analyze the possibilities and limitations of using additive manufacturing to create high-tech components of engines with variable specific impulse. The research methodology is based on an interdisciplinary approach using mathematical modeling of heat transfer processes, optimization of the geometry of engine elements and analysis of physical and mechanical properties of materials suitable for SLM, DED and EBM technologies. As a result of the research, it was proven that the use of additive technologies allows creating light, strong and heat-resistant structures with variable geometry, capable of providing variations in thrust and increasing specific impulse. The key conclusion is the expediency of introducing additive manufacturing as a tool for forming adaptive rocket engines of a new generation and developing the innovative potential of domestic engine engineering. At the same time, Additive technologies in Ukraine have already begun to be implemented in the production of rocket engines with variable specific impulse, mostly at the stage of prototyping and manufacturing of individual complex parts. Despite the significant challenges associated with economic restrictions, military actions and technological dependence on imports, the prospects for the development of this industry are strong. To achieve sustainable progress, it is necessary to focus on the localization of production, the development of the scientific and technical base, the training of highly qualified personnel and the introduction of digital tools into production processes. Such a comprehensive approach will allow to increase the technological independence of Ukraine, strengthen the defense capability and ensure competitiveness at the international level in the conditions of modern challenges
References
Adzhamskyi, S. V., Kononenko, H. A., & Podolskyi, R. V. (2021). Vyhotovlennia traktu okholodzhennia vdoskonalenoi konstruktsii dlia kamery zghoriannia ridynnoho raketnoho dvyhuna za dopomohoiu adytyvnykh tekhnolohii. Aerospace Technic and Technology, (3), 42–48. https://doi.org/10.32620/aktt.2021.3.05
Blachowicz, T., Ehrmann, G., & Ehrmann, A. (2021). Metal additive manufacturing for satellites and rockets. Applied Sciences, 11(24), 12036. https://doi.org/10.3390/app112412036
Buchholz, M., Gruber, S., Selbmann, A., Marquardt, A., Meier, L., Müller, M., Seifert, L., Leyens, C., Tajmar, M., & Bach, C. (2022). Flow rate improvements in additively manufac-tured flow channels suitable for rocket engine application. CEAS Space Jour-nal. https://doi.org/10.1007/s12567-022-00476-7
Cheng, C., Wang, Y., Liu, Y., Liu, D., & Lu, X. (2013). Thermal-structural response and low-cycle fatigue damage of channel wall nozzle. Chinese Journal of Aeronautics, 26(6), 1449–1458. https://doi.org/10.1016/j.cja.2013.07.045
Chowdhury, S., Yadaiah, N., Prakash, C., Ramakrishna, S., Dixit, S., Gulta, L. R., & Bud-dhi, D. (2022). Laser powder bed fusion: A state-of-the-art review of the technology, materi-als, properties & defects, and numerical modelling. Journal of Materials Research and Tech-nology. https://doi.org/10.1016/j.jmrt.2022.07.121
Ciochon, A., & Kennedy, J. (2024). Efficient modelling of surface roughness effects in ad-ditively manufactured materials. Applied Acoustics, 220, 109953. https://doi.org/10.1016/j.apacoust.2024.109953
Cui, Z. (2025). Metal additive manufacturing technology in rocket engines and future pro-spects. Applied and Computational Engineering, 156(1), 99–103. https://doi.org/10.54254/2755-2721/2025.mh25251
da Silva Couto, H., Lacava, P. T., Bastos-Netto, D., & Pimenta, A. P. (2009). Experimental evaluation of a low pressure-swirl atomizer applied engineering design procedure. Journal of Propulsion and Power, 25(2), 358–364. https://doi.org/10.2514/1.37018
Gradl, P. R., & Protz, C. S. (2020). Technology advancements for channel wall nozzle manufacturing in liquid rocket engines. Acta Astronautica, 174, 148–158. https://doi.org/10.1016/j.actaastro.2020.04.067
Grefen, B., Becker, J., Linke, S., & Stoll, E. (2021). Design, production and evaluation of 3d-printed mold geometries for a hybrid rocket engine. Aerospace, 8(8), 220. https://doi.org/10.3390/aerospace8080220
Ha, D., Roh, T.-S., Huh, H., & Lee, H. J. (2022). Development trend of liquid hydrogen-fueled rocket engines (part 2: Core technologies). International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-022-00518-8
Hong, M., Jeon, J., & Lee, S. Y. (2012). Discharge coefficient of pressure-swirl atomizers with low nozzle opening coefficients. Journal of Propulsion and Power, 28(1), 213–218. https://doi.org/10.2514/1.b34168
Immich, H., Alting, J., Kretschmer, J., & Preclik, D. (2003). Technology developments for thrust chambers of future launch vehicle liquid rocket engines. Acta Astronautica, 53(4-10), 597–605. https://doi.org/10.1016/s0094-5765(03)80021-8
Kadivar M., Tormey D., McGranaghan G. CFD of roughness effects on laminar heat trans-fer applied to additive manufactured minichannels. Heat and Mass Transfer. 2022. URL: https://doi.org/10.1007/s00231-022-03268-1
Kang, Z., Wang, Z.-g., Li, Q., & Cheng, P. (2018). Review on pressure swirl injector in liquid rocket engine. Acta Astronautica, 145, 174–198. https://doi.org/10.1016/j.actaastro.2017.12.038
Kaynak, Y., Tascioglu, E. Post-processing effects on the surface characteristics of Inconel 718 alloy fabricated by selective laser melting additive manufacturing. Progressin Additive Manufacturing, 2020, vol. 5, pp. 221–234. DOI: 10.1007/s40964-019-00099-1.
Kim, H., et al. (2024). Preliminary Design of 35tonf Methane Combustion Chamber for Additive Manufacturing. KSPE, 28(2), 83–96. DOI: 10.6108/KSPE.2024.28.2.083
Kuntanapreeda, S., & Hess, D. (2020). Opening access to space by maximizing utilization of 3D printing in launch vehicle design and production. Applied Science and Engineering Progress, 14(2). https://doi.org/10.14416/j.asep.2020.12.002
Kuts, D., Yefanov, V., Halienkova, O., Ovchynnykov, O., Tepla, T., Lemishka, I., & Mierzwiński, D. (2025). Additive technologies for manufacturing swirlers of the combustion chamber of aircraft engines from nickel superalloy powders. Archives of Materials Science and Engineering. https://doi.org/10.5604/01.3001.0055.0368
Lee, K. O., et al. (2023). New Space 3D Printing Rocket Engine Development Trends. JKSP Engineers, 27(3), 63–77. DOI: 10.6108/KSPE.2023.27.3.063
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