image: Figure 1. (From left) Prof. Sung-Hoon Ahn and Dr. Jun Young Choi of SNU Department of Mechanical Engineering standing on a 300 g composite beam developed in this study that supports a total load of approximately 150 kg; prototype structures developed by the research team (drone, robotic arm)
Credit: © Seoul National University College of Engineering
Seoul, South Korea — Researchers at Seoul National University have developed a new class of ultralight structural materials that combine the load-bearing strength of engineering materials with the weight of foam. Using a method called 3D node winding, the team created mesoscale carbon fiber lattices that achieve aluminum-level performance on a strength-to-weight basis while weighing as little as 1/100 the weight of aluminum. The findings, published in Nature Communications, demonstrate a new way to build strong, lightweight structures without the need for joints or layered assembly.
The approach removes one of the key bottlenecks in structural design: the need to assemble complex three-dimensional forms from discrete parts. Instead, structures are created as continuous systems, enabling both geometric complexity and mechanical integrity to be achieved simultaneously.
Rethinking how strong structures are made
Strong, lightweight materials are essential in applications ranging from drones and robots to vehicles and aerospace systems. Today’s carbon fiber composites already offer high strength at low weight, but they are typically manufactured by stacking thin layers or assembling multiple components. These processes limit design freedom and introduce weak interfaces where layers or parts meet.
Even newer approaches, such as 3D-printed composites, rely on layer-by-layer fabrication. This creates internal boundaries that disrupt load transfer, forcing a trade-off between structural complexity and mechanical reliability.
Building structures from a single continuous fiber
To overcome these limitations, the research team turned to a fundamentally different fabrication strategy—one that marks the true starting point of the new approach: instead of assembling or stacking materials, the structure is defined by placing a single continuous carbon fiber directly in three-dimensional space, a unifying concept that “binds them all together in perfect unity.”
The process begins with a temporary scaffold that defines nodal geometry. A long carbon fiber is then wound across these nodes, forming a spatial lattice network. Once the geometry is established, the structure is consolidated through resin impregnation, producing a solid composite.
Because the fiber remains continuous throughout the structure, forces are transmitted without interruption, avoiding the stress concentrations and failure points commonly associated with joints and interfaces.
High strength at ultralow weight
The resulting structures exhibit compressive strengths of approximately 10 to 30 megapascals, comparable to construction-grade materials such as concrete in compression. While this remains below the absolute strength of high-grade metals, the structures achieve exceptional performance when normalized by weight, reaching aluminum-level efficiency at dramatically reduced mass.
At equal weight, the lattices can be up to ten times stronger than conventional lattice structures. This improvement arises from continuous load paths, which enable more efficient force distribution and reduce inactive material within the structure.
Demonstrated in a flying drone
To validate the approach in a real-world system, the researchers applied the structure to a drone frame. The redesigned frame reduced structural weight by approximately 79 percent compared to conventional designs. This reduction directly resulted in a 33 percent increase in flight time under the same operating conditions.
These results confirm that structural weight reduction translates directly into improved system-level performance, particularly in applications where mass is a primary constraint.
Toward scalable, design-driven structures
Beyond material performance, the work reframes how load-bearing systems can be designed and manufactured. Rather than relying on assembly or layering, the approach enables structures to be defined through continuous fiber paths, allowing geometry and load distribution to be optimized together.
Previously, such continuous three-dimensional fiber architectures were difficult to scale using conventional manufacturing methods. However, this approach aligns naturally with robotic, toolpath-driven fabrication systems, where complex fiber trajectories can be generated and executed directly from digital designs. As these systems advance, they are expected to enable scalable production of architected composites that would be impractical to fabricate by hand.
“The spatial complexity of continuous fiber architectures has limited their scalability in conventional manufacturing,” said Dr. Jun Young Choi and Prof. Sung-Hoon Ahn. “With advances in robotic and AI-driven fabrication, these structures can now be produced at scale, and this work provides a roadmap for their practical realization.”
The implications extend across multiple industries where weight and efficiency are critical. In aerospace and mobility systems, reducing structural mass improves range, payload capacity, and energy efficiency. In robotics, lightweight yet stiff structures enable faster actuation and improved precision. In construction, the approach opens pathways for material-efficient load-bearing frameworks that reduce material usage while maintaining structural integrity. More broadly, the method supports a transition from component-based engineering to integrated structural systems defined by geometry, continuity, and automated fabrication.
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Method of Research
Experimental study
Subject of Research
Not applicable
Article Title
Mesoscale carbon fiber lattices with foam-like weight and bulk strength
Article Publication Date
21-Apr-2026
COI Statement
J.Y.C. and S.-H.A. are inventors on patent applications related to the work reported in this manuscript. These include a Korean patent application (No. 10-2025-0050584, filed April 18, 2025) and an international PCT application (PCT/KR2025/095742, filed November 19, 2025), as well as corresponding national-phase applications in multiple jurisdictions, including the United States (Application No. 19/500,340, filed January 8, 2026), China (Application No. 202580003964.8, filed February 2, 2026), Japan (Application No. 2026-019459, filed February 9, 2026), and Europe (Application No. 25841815.1, filed January 26, 2026). All applications are currently pending examination. The other authors declare no competing interests.