AFRL Flight Research Vehicle Designated X-56A | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-07.14.25

Airborne-NextGen-07.15.25

AirborneUnlimited-07.16.25

Airborne-FlightTraining-07.17.25

AirborneUnlimited-07.11.25

Mon, Mar 05, 2012

AFRL Flight Research Vehicle Designated X-56A

UAV Will Be Used In Aircraft Configuration Research

The Air Force Research Laboratory was recently awarded an X-Plane designation for a vehicle that will be used to explore active control of lightweight, aerodynamically-efficient aircraft configurations. The X-56A is an innovative, modular, unmanned fight research vehicle that will allow investigation of active flutter suppression and gust load alleviation technology.

Flutter is an instability that can occur when unsteady aerodynamic loads acting on a wing couple with its natural vibration modes, often resulting in catastrophic failures. The research to be conducted with the X-56A is critical for the successful development of future slender, lightweight, high aspect ratio wing designs that could be used by energy efficient transport and unmanned aircraft.

The X-56A, also known as the Multi-Utility Technology Testbed (MUTT) flight demonstrator, is a product of the AFRL-led Multi-Utility Aeroelastic Demonstration (MAD) program. This program is a joint effort between AFRL's Air Vehicles Directorate, NASA Dryden and Lockheed Martin.

The X-56A is powered by twin JetCat P240 turbojets, has a 28-foot wing span, weighs 480 pounds, and is designed and constructed for easy wing replacement to enable testing of various flexible wing configurations. An additional hard point is being designed into the center of aft upper deck of the fuselage for mounting an additional third engine or a structural member to support testing of joined wing configurations. These characteristics will allow the testing of a wide range of advanced aerodynamic concepts. The X-56A will exhibit multiple rigid body and aeroelastic instabilities within its flight envelope, which will be actively managed by its flight control system.

The first X-56A flight is scheduled for summer 2012. Following Air Force flight testing, the X-56A will be used by NASA's Dryden Flight Research Center for their continuing research into lightweight structures and advanced technologies for future low-emissions transport aircraft.

FMI: www.af.mil

Advertisement

More News

ANN's Daily Aero-Term (07.15.25): Charted Visual Flight Procedure Approach

Charted Visual Flight Procedure Approach An approach conducted while operating on an instrument flight rules (IFR) flight plan which authorizes the pilot of an aircraft to proceed >[...]

Aero-News: Quote of the Day (07.15.25)

“When l became the Secretary of Defense, I committed to rebuild our military to match threats to capabilities. Drones are the biggest battlefield innovation in a generation, >[...]

ANN's Daily Aero-Linx (07.15.25)

Aero Linx: Stearman Restorers Association Welcome to the Stearman Restorers Association. The Stearman Restorers Association is an independent “Not for Profit” 501C-3 Co>[...]

NTSB Final Report: Kjelsrud Gary Kitfox

Airplane Exhibited A Partial Loss Of Engine Power When It Was About Halfway Down The Runway Analysis: The pilot of the experimental amateur-built airplane was departing from his pr>[...]

NTSB Prelim: Cessna A150L

The Flight Path Was Consistent With Low-Altitude Maneuvering On June 18, 2025, about 0922 mountain standard time, a Cessna A150L airplane, N6436F, was substantially damaged when it>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC