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5.5%: The Path to Achieving Over 30% Room-Temperature Plasticity in CuCrNb-42 via SLM + HIP
Release date:
2026-04-16
Author:
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Abstract
01 [King of Data]
CuCrNb-42, which combines high thermal conductivity with excellent high‑temperature strength, is a key heat‑dissipating material for the combustion chamber liners of next‑generation aerospace engines and can be fabricated via SLM followed by HIP, or by direct HIP forming. However, its drawback is also quite apparent: the material typically exhibits relatively low room‑temperature elongation.
Through optimization of powder processing, refinement of SLM validation parameters, and exploration of HIP procedures, Asia Materials has successfully increased the room-temperature ductility of CuCrNb-42 to over 30% under the SLM+HIP process route, while the material also exhibits higher strength than that specified in NASA’s supply chain standards. Detailed data are provided in Table 1, and the material’s tensile performance is shown in Figure 1.
Table 1 Typical Test Properties of CuCrNb-42 from Different Manufacturers (SLM + HIP Process)



Figure 1: Mechanical Property Report for the CuCrNb-42 SLM+HIP Process
02 [What does 35.5% mean?]
In high-strength, high-conductivity copper alloy systems, achieving a room-temperature elongation exceeding 30% is widely recognized as a critical technical threshold. This implies:
• The material’s crack‑resistance and in-service reliability have been significantly enhanced;
• Offers a greater safety margin under complex stress conditions;
• It provides a more robust material foundation for the fabrication of large‑size, thin‑walled components with complex internal flow channels.
03 [What We Did]
Our high-quality CuCrNb-42 spherical powder boasts the following characteristics:
• Excellent compositional uniformity and flowability, with stable powder spreading performance.
• Low oxygen content effectively reduces the risk of oxidized inclusions.
• Uniform particle size distribution ensures high density of printed parts.
More importantly, we collaborate closely with our customers—spanning everything from upstream powder‑quality control and print‑parameter optimization to process validation for HIP post‑processing—thus establishing a fully integrated closed‑loop system. Achieving a room‑temperature ductility of 35.5% is no accident; it is the inevitable outcome of seamless synergy among powder formulation, process parameters, and post‑processing techniques.

04 [The Future Has Arrived]
While the aerospace market is focused on supplying the current-generation high‑strength, high‑conductivity material—CuCrZr—this breakthrough has validated the suitability of a new generation of high‑strength, high‑conductivity copper alloys, such as CuCrNb‑42, for applications in aerospace engine combustion chambers and thermal protection structures of hypersonic vehicles, demonstrating that downstream manufacturing can fully meet the design requirements. We also look forward to collaborating with more customers to further unlock the potential of the SLM+HIP process.
Furthermore, the latest results of this project suggest that the low‑cost powder‑plus‑As‑HIP route also holds significant technical potential in this field. Coarse powders exhibit slower cooling rates and more challenging control over compositional uniformity; however, through process optimization and property characterization, it has been demonstrated that even coarse powders can achieve the compositional homogeneity required for HIP. Figure 2 shows the measured uniform dispersion of the Cr₂Nb phase within the powder.


Figure 2: Uniform distribution of the Cr2Nb phase in the 53–150 μm powder.
For inquiries about CuCrNb-42 powder products or technical documentation, please contact us.
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