With the use of composite (non-metallic) and microelectronics becoming more prevalent in the construction of both military and commercial aircraft, the control systems have become more susceptible to damage or failure from electromagnetic transients. One source of such transients is the lightning discharge. In order to study the effects of the lightning discharge on the vital components of an aircraft, NASA Langley Research Center has undertaken a Storm Hazards Program in which a specially instrumented F106B jet aircraft is flown into active thunderstorms with the intention of being struck by lightning. One of the specific purposes of the program is to quantify the environmental conditions which are conductive to aircraft lightning strikes
Transmission loss from precipitation scatter interference between space and earth communication syst...
Preliminary flight tests with a F-106B aircraft were made on the periphery of isolated thunder cells...
An analytical model for calculation of ascent steady state tile loading was developed and validated ...
As part of the NASA Langley Research Center Storm Hazards Program, 69 thunderstorm pentrations were ...
Work accomplished during this period centered on the completion of the first order parameterization ...
Present practices in lightning protection of aircraft deal primarily with the direct effects of ligh...
Lightning has always been of concern for aerospace vehicle ground activities. The unexpected trigger...
Test program for measuring electric fields inside clouds by rocket induced artificial lightnin
Developments in the use of space related techniques to understand storms and local weather are summa...
The Nighttime/Daytime Optical Survey of Lightning experiment was selected for flight on Orbital Flig...
Thunderstorm days at KSC; percentage of frequency of thunderstorms (1957-1989); effect of lightning ...
NASA's program in aircraft icing research and technology is reviewed. The program relies heavily on ...
Low-altitude wind shear is recognized as an infrequent but significant hazard to all aircraft during...
The ambient trapped particle fluxes incident on the IUE (SAS-D) satellite were studied. Several sync...
The goal of the F106B Thunderstorm Research Program is to characterize the lightning environment for...
Transmission loss from precipitation scatter interference between space and earth communication syst...
Preliminary flight tests with a F-106B aircraft were made on the periphery of isolated thunder cells...
An analytical model for calculation of ascent steady state tile loading was developed and validated ...
As part of the NASA Langley Research Center Storm Hazards Program, 69 thunderstorm pentrations were ...
Work accomplished during this period centered on the completion of the first order parameterization ...
Present practices in lightning protection of aircraft deal primarily with the direct effects of ligh...
Lightning has always been of concern for aerospace vehicle ground activities. The unexpected trigger...
Test program for measuring electric fields inside clouds by rocket induced artificial lightnin
Developments in the use of space related techniques to understand storms and local weather are summa...
The Nighttime/Daytime Optical Survey of Lightning experiment was selected for flight on Orbital Flig...
Thunderstorm days at KSC; percentage of frequency of thunderstorms (1957-1989); effect of lightning ...
NASA's program in aircraft icing research and technology is reviewed. The program relies heavily on ...
Low-altitude wind shear is recognized as an infrequent but significant hazard to all aircraft during...
The ambient trapped particle fluxes incident on the IUE (SAS-D) satellite were studied. Several sync...
The goal of the F106B Thunderstorm Research Program is to characterize the lightning environment for...
Transmission loss from precipitation scatter interference between space and earth communication syst...
Preliminary flight tests with a F-106B aircraft were made on the periphery of isolated thunder cells...
An analytical model for calculation of ascent steady state tile loading was developed and validated ...