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Meeting 2026 TMS Annual Meeting & Exhibition
Symposium Advanced Materials for Reusable Rocket Engines
Presentation Title Wire-Arc AM Combustion Chambers: Reusability Considerations with AM and Accelerating the Material Development Path to Flight
Author(s) Bishop Wright, Jeff Rossin, Jamie Cleland
On-Site Speaker (Planned) Bishop Wright
Abstract Scope Building off the Terran-1 launch, Relativity Space has taken the next step with wire-arc (WAAM) and powder bed fusion (PBF) additive manufacturing (AM) processes in fracture critical applications. Terran-R, our next-generation reusable rocket, utilizes an additively manufactured Main Combustion Chamber (MCC) for the Aeon-R engine. With the need for reusable engines, a variety of material-process challenges arise concurrent with the need for rapid developmental iteration and engine component testing. This talk will center on the use of WAAM nickel alloys for the structural features of the MCC throughout Aeon-R development and qualification, focusing on the interaction of material structure and properties with engine performance, developmental risk posture, repair/ inspect-ability challenges, and timeline to achieve engine test objectives. The challenges with the implementation of novel technical solutions such as alloy improvements and feedstock availability will be presented to the community at large.
Proceedings Inclusion? Planned:
Keywords Additive Manufacturing, Copper / Nickel / Cobalt, Other

OTHER PAPERS PLANNED FOR THIS SYMPOSIUM

Approach to Oxygen Compatibility - Material Selection and Testing for Lower Cost to Orbit
Characterization of Additively Manufactured MA754 Contaminates for Compositional Optimization
Disruption of Oxide Barriers in Reaction Bonded, 3D Printed Ceramics via Surface-Applied In–Ga Eutectic
Frictional Ignition Testing of Metals in Oxygen up to 24.1 MPa
HVOF Thermal Spray Additively Manufacturing Processing of GRX-810 Alloy for Scalable Rocket Engine Components
Microstructural and Mechanical Characterization of Nano-Yttria Reinforced IN718 via L-PBF
Property-driven design of compositionally graded alloys using a generative AI framework
Temperature-Dependent Effects in the Aeroplastic Design of Turbine Disks
Using ICMDŽ Software to Design High Strength, Printable, Burn Resistant Nickel-Based Superalloys for Reusable Rocket Engines
Wire-Arc AM Combustion Chambers: Reusability Considerations with AM and Accelerating the Material Development Path to Flight

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