Development of metallic transition joints for space propulsion systems applications

• Published in: CEAS space journal 2023, Vol.15 (1), p.169-181
• Main Authors: Carrolo, E., Fernandes, N., Trigueiro, J., Lourenço, F., Salles, R., Pereira, D., Norman, A.
• Format: Article
• Language: English
• Subjects: Aerospace Technology and Astronautics; Aluminum; Carbon fiber reinforced plastics; Carbon fibers; Confidence intervals; Configurations; Contact force; Diameters; Discharge; Elastic deformation; Engineering; Friction welding; Impact damage; Original Paper; Propulsion systems; Stainless steel; Stainless steels; Thickness; Titanium; Transition joints; Tube joints; Tubes
• ISSN: 1868-2502; 1868-2510
• DOI: 10.1007/s12567-021-00420-1

Two technologies, rotary friction welding and magnetic pulse welding/forming, have been developed to produce joints in various metal–metal and metal–non-metal combinations. For the rotary friction welding process, the techniques have been successfully developed to allow high-quality reliable joints for both titanium–stainless steel and titanium–aluminium combinations. The titanium–stainless steel configuration has reached a high level of maturity such that since the final qualification was achieved, about 200 flight units have been manufactured and sold in the last 11 years, with a steady demand over time. This includes ten configurations and two different families concerning length, wall thickness and outer diameter. For the titanium–aluminium transition joint, development and qualification activities were successfully performed in three different geometries: 1 4 ″ , 3 8 ″ , and 1 2 ″ . The testing campaigns were designed to seek the performance limits of the units and this allowed an improved understanding and higher confidence level of the final product. For the challenge of obtaining a reliable join between metals and non-metals, the production of aluminium to carbon fibre tube joints was achieved with the MPW technology. From the obtained results, the friction-based model for the joint was confirmed, and it was also possible to conclude that the discharge energy plays a critical role in the joint strength. It was also observed that to maintain the same joint strength, the discharge energy needs to be increased when the flyer wall thickness and joint diameter are also increased. Furthermore, the gap to the aluminium mandrel, corresponding to the admissible deformation possible to impose within the elastic regime of these tubes, should not only be considered to avoid damaging the CFRP tubes with the impact/deformation, but can also be used as a control parameter for the joint resistance, since it is this elastic deformation that in part determines the contact force between the two materials. This technology proved to be a viable approach to performing 40 mm diameter tubular joints between aluminium and CFRP tubes. However, for a full characterization of the effect of the discharge energy on the joint strength, it is necessary to produce more samples to establish a trend, as well as confirming its reproducibility.