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X-56A

Product descripton: X-56A by Lockheed Martin

The X‑56A is a modular research unmanned aerial vehicle developed by Lockheed Martin’s Skunk Works in collaboration with the U.S. Air Force Research Laboratory and NASA. It is designed to investigate high-altitude, long-endurance flight by testing advanced aeroelastic control technologies such as active flutter suppression and gust-load alleviation using interchangeable stiff and highly flexible wings. The platform enables evaluation of lightweight, high-aspect-ratio wing configurations that would typically be prone to flutter. Testing included both stiff and flexible wing sets to validate digital flight control suppression across various instability modes.

Technical specifications

Category Specification
Length 2.3 m (7.5 ft)
Wingspan 8.4 m (27.5–28 ft)
Weight (Empty) Approx. 220 kg (480 lb)
Powerplant 2 × JetCat P400 turbojets (~89 lbf thrust each)
Maximum Speed ~222 km/h (138 mph / 120 knots)
Flutter Test Speed ~200 km/h (110 knots)
Wing Configurations Stiff wings + flexible wings (four pairs built for testing)
Flight Control System Digital active flutter suppression (including body‑freedom flutter)
Recovery System Ballistic parachute for safe recovery after wing failure

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