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Advanced 3D additive manufacturing techniques for revolutionizing the next-generation rocket engine nozzle fabrication

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Abstract

The aim of this study was to evaluate the redesign and additive manufacturing of a rocket engine nozzle using Inconel 625 material. The redesigned engine took into consideration material shrinkage during the metal transfer process. The additive manufacturing process was carried out using the appropriate toolpaths to form a solid structure. Micrographs of the additively manufactured structure showed layer resolution and fine detail, as well as the presence of metallic particles within the polymer matrix. The final rocket engine nozzle produced was found to have the necessary mechanical and metallurgical properties required for practical use in future space vehicle operations. This was demonstrated by tensile tests carried out at various temperatures and 3D white light interferometry scans of the surface properties. The results of the study suggest that additive manufacturing and Inconel 625 material can be used to produce high-performance rocket engine nozzles that meet the requirements of the aerospace industry. This study provides valuable insights into the potential applications of additive manufacturing in the aerospace industry and may lead to the development of new, high-performance rocket engine nozzles.

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There are no current confirm of interested to declare. The author wrote the manuscript, prepared the images, and carried out the scientific work over the course of 3 years.

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Correspondence to Daniel J. Thomas.

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Thomas, D.J. Advanced 3D additive manufacturing techniques for revolutionizing the next-generation rocket engine nozzle fabrication. Int J Adv Manuf Technol 127, 3747–3760 (2023). https://doi.org/10.1007/s00170-023-11669-7

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