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Boeing X-53 AAW (Active Aeroelastic Wing)

United States (2006)

Detailing the development and operational history of the Boeing X-53 AAW (Active Aeroelastic Wing) Experimental Aircraft.

 Entry last updated on 7/11/2016; Authored by Staff Writer; Content ©www.MilitaryFactory.com



  Boeing X-53 AAW (Active Aeroelastic Wing)  
Picture of Boeing X-53 AAW (Active Aeroelastic Wing) Experimental Aircraft


The Boeing X-53 AAW is based on the FA-18 Hornet series fighter with all-new wing technology.

There are currently no development or operational history details available for the Boeing X-53 AAW (Active Aeroelastic Wing) Experimental Aircraft. Rest assured that we are hard at work on adding the required information to the Military Factory database to complete this particular entry in full so please check back at a future date.

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Any available statistics for the Boeing X-53 AAW (Active Aeroelastic Wing) Experimental Aircraft are showcased in the areas immediately below. Categories include basic specifications covering country-of-origin, operational status, manufacture(s) and total quantitative production. Other qualities showcased are related to structural values (namely dimensions), installed power and standard day performance figures, installed or proposed armament and mission equipment (if any), global users (from A-to-Z) and series model variants (if any).
Boeing X-53 AAW Specifications
National Flag Graphic
United States
Year: 2006
Type: Experimental Aircraft
Manufacturer(s): Boeing Company / McDonnell Douglas / Northrop Grumman / NASA - USA
Production: 1
Supported Mission Types
Air-to-Air
Interception
Unmanned
Ground Attack
Close-Air Support
Training
Anti-Submarine
Anti-Ship
Airborne Early Warning
MEDEVAC
Electronic Warfare
Maritime/Navy
Aerial Tanker
Utility/Transport
Passenger Industry
VIP Travel
Business Travel
Search/Rescue
Recon/Scouting
Special Forces
X-Plane/Development
Structural
Crew: 1
Length: 56.10 ft (17.1 m)
Width: 38.39 ft (11.70 m)
Height: 15.26 ft (4.65 m)
MTOW: 39,022 lb (17,700 kg)


Installed Power
2 x General Electric F404-GE-400 turbofan engines developing 16,000 lb of thrust each.

Standard Day Performance
Maximum Speed: 1,190 mph (1,915 kph; 1,034 kts)
Maximum Range: 1,864 mi (3,000 km; 1,620 nm)
Service Ceiling: 49,213 ft (15,000 m; 9.32 mi)
Rate-of-Climb: 50,000 ft/min (15,240 m/min)


Armament
None.

Operators List
United States

Series Model Variants
• X-53 - Base Product Designation; single example completed from F/A-18 airframe.