The status of the Airborne Warning and Avoidance System 3 (AWAS 3) is reported in viewgraph form. Information is given on flight tests and FAA certification. Included is a description of the flight test of a passive infrared system that achieved the first ever advanced warning of an in-flight windshear encounter. The infrared system recorded the detection of the windshear with a 35 second advance warning. The data recorded in-flight by the infrared system was later compared to and found to agree with the data recorded by the Terminal Doppler Weather Radar (TDWR) and the in-situ air data
Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft ...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
Aircraft tracking and guidance facility using FPS-16 radar supplemented by laser tracker permanently...
The feasibility of infrared optical techniques for the advance detection and avoidance of low level ...
Preliminary designs and the supporting analysis for both the Aeromaneuvering Orbit-to-Orbit Shuttle ...
The isothermal fatigue damage and life behaviors of SCS-6/Timetal 21S (0/90)s were investigated at 6...
Transmission loss from precipitation scatter interference between space and earth communication syst...
Structural dynamic environmental test levels were developed for the thematic mapper instrument, comp...
The detection of clear-air turbulence (CAT) ahead of an aircraft in real-time by an infrared (IR) ra...
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
The current techniques of helicopter rotor noise prediction attempt to describe the details of the n...
The nondestructive testing (NDT) on the Space Shuttle Solid Rocket Booster (SRB) filament wound case...
Analysis was made to determine characteristics required of a balancing-tab system for ailerons in or...
The NASA Lewis Research Center and the U.S. Army Aviation Systems Command share an interest in advan...
Several approaches to develop a diagnostics system for monitoring the operational health of the Spac...
Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft ...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
Aircraft tracking and guidance facility using FPS-16 radar supplemented by laser tracker permanently...
The feasibility of infrared optical techniques for the advance detection and avoidance of low level ...
Preliminary designs and the supporting analysis for both the Aeromaneuvering Orbit-to-Orbit Shuttle ...
The isothermal fatigue damage and life behaviors of SCS-6/Timetal 21S (0/90)s were investigated at 6...
Transmission loss from precipitation scatter interference between space and earth communication syst...
Structural dynamic environmental test levels were developed for the thematic mapper instrument, comp...
The detection of clear-air turbulence (CAT) ahead of an aircraft in real-time by an infrared (IR) ra...
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
The current techniques of helicopter rotor noise prediction attempt to describe the details of the n...
The nondestructive testing (NDT) on the Space Shuttle Solid Rocket Booster (SRB) filament wound case...
Analysis was made to determine characteristics required of a balancing-tab system for ailerons in or...
The NASA Lewis Research Center and the U.S. Army Aviation Systems Command share an interest in advan...
Several approaches to develop a diagnostics system for monitoring the operational health of the Spac...
Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft ...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
Aircraft tracking and guidance facility using FPS-16 radar supplemented by laser tracker permanently...