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Flight Loads Laboratory Quick Facts

Structural Loads Testing on F/A-18 AAW Aircraft
Structural loads testing on the Active Aeroelastic Wing F-18 in the Flight Loads Laboratory at NASA’s Dryden Flight Research Center, Edwards, CA.
NASA

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Flight Loads Laboratory Quick Facts

The FLL supports a broad spectrum of flight-research programs from NASA, DoD, private industry, aerospace organizations and academia.

With its accessibility to the Rogers Dry Lake and the Edwards Air Force Base flight line, the FLL is ideally suited to conduct structural tests on a wide variety of experimental vehicles.

Main High Bay Size
164 ft wide x 120 ft deep x 40 ft high

Aircraft Access
Direct access via DFRC and EAFB taxiways and runways including Rodgers Dry Lakebed

Mechanical Load
Up to 84 channels hydraulic load control with maximum loads up to ±300,000 lbs

Thermal Testing
-320° F to >3,000° F

Follow flight temperature time histories using quartz lamp and graphite heating systems configured in independent control zones.

Structural Dynamics Testing
Modal survey and structure/control mode interaction testing of aircraft and components.

Flight Research Facilities

Flight Demonstrations and Capabilities Project

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Last Updated
Jul 23, 2023
Editor
Lillian Gipson
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