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Adaptive Aerodynamic Surface Actuation System for Hypersonic Aircraft Stabilization

Patent #US13510889B2

Public record:Verify on Google Patents

A morphing wing structure using shape-memory alloys to adjust curvature during high-velocity maneuvers. The system compensates for fluctuating thermal loads to maintain aerodynamic efficiency at Mach 5+ speeds.

Issue Date

4/22/2026

Inventor

Dr. Hiroshi Tanaka

Seller Location

United States

Price on request

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