|Dryden Home > Collections > Movie Home > F-15B > Movie EM-0078-03|
Lifting Insulating Foam Trajectory (LIFT) flight test closeup
|Formats:||160x120 QuickTime Movie (.1 MB)
320x240 QuickTime Movie (.4 MB)
480x320 QuickTime Movie (.9 MB)
640x480 QuickTime Movie (1.5 MB)
|Still photos of the F-15B are available in several resolutions at http://www.nasa.gov/centers/dryden/multimedia/imagegallery/F-15A/index.html|
This 9 second movie clip shows a closeup of the Lifting Insulating Foam Trajectory (LIFT) flight test.
Flight research carried out by NASA with a highly modified F-15 aircraft demonstrated and evaluated advanced integrated flight and propulsion control system technologies that will help make next-generation aircraft more maneuverable, more fuel efficient, and safer to fly.
The NASA F-15 was the first aircraft to demonstrate a fully integrated inlet-engine-flight control system, a self-repairing flight control system, and a propulsion-only flight control system.
The F-15 was designed as twin-engine air superiority fighter by McDonnell Aircraft Co., McDonnell Douglas Corporation, St. Louis, Missouri. The F-15 is normally powered by two Pratt and Whitney F100-PW-100 or 220 engines, depending on the model. The NASA F-15 was equipped with advanced versions of the F100 -- F100 EMD (engine model derivative).
The aircraft was capable of flying more than twice the speed of sound. The F-15 is 63.75 feet long and has a wingspan of 42.83 feet. The NASA F-15 was extensively modified for research activities and did not carry any armament.
|Keywords||F-15B, Lifting Insulating Foam Trajectory (LIFT) Flight Test closeup