The results of the inspection and analysis of two F-106A aircraft that were struck by separate lightning strikes within a few minutes of each other are presented. Each aircraft sustained severe lightning strikes to the pitot booms, resulting in extensive damage to the pitot heater power harness, number 8 ground wire, and lightning suppressors, but there was no damage to either aircraft's electrical or avionic systems. A simulated lightning current of 226 kA and 3.8 million A(2)*S was required to reproduce the damage to the ground wires in the radomes. Photographs and detailed assessments of the damage are included
The current knowledge concerning potential lightning effects on aircraft and the means that are avai...
Data waveforms are presented which were obtained during the 1983 direct strike lightning tests utili...
Various characteristics of the electromagnetic data obtained on a NASA F-106B aircraft during direct...
A highly instrumented NASA F-106B aircraft, modified for the storm hazards mission and protected aga...
The damage sustained by a Beechcraft King Air Model B90 aircraft by a single lightning discharge is ...
Ground-based data collected on lightning monitoring equipment operated by Goddard Space Flight Cente...
Preliminary flight tests with a F-106B aircraft were made on the periphery of isolated thunder cells...
As part of the NASA Langley Research Center Storm Hazards Program, 241 thunderstorm penetrations wer...
The NASA F-106 collected data on the rates of change of electromagnetic parameters on the aircraft s...
As part of the NASA Langley Research Center Storm Hazards Program, 69 thunderstorm pentrations were ...
During the Storm Hazards Experiment 1982, the Goddard Space Flight Center monitored radiation from l...
Data waveforms obtained during the 1981 direct strike lightning tests, utilizing the NASA F-106B air...
Tests designed to investigate the lightning-generated electromagnetic environment affecting aircraft...
Data waveforms are presented which were obtained during the 1985 and 1986 direct-strike lightning te...
The triggered lightning environment of the F106B aircraft is investigated. Scale modeling of the F10...
The current knowledge concerning potential lightning effects on aircraft and the means that are avai...
Data waveforms are presented which were obtained during the 1983 direct strike lightning tests utili...
Various characteristics of the electromagnetic data obtained on a NASA F-106B aircraft during direct...
A highly instrumented NASA F-106B aircraft, modified for the storm hazards mission and protected aga...
The damage sustained by a Beechcraft King Air Model B90 aircraft by a single lightning discharge is ...
Ground-based data collected on lightning monitoring equipment operated by Goddard Space Flight Cente...
Preliminary flight tests with a F-106B aircraft were made on the periphery of isolated thunder cells...
As part of the NASA Langley Research Center Storm Hazards Program, 241 thunderstorm penetrations wer...
The NASA F-106 collected data on the rates of change of electromagnetic parameters on the aircraft s...
As part of the NASA Langley Research Center Storm Hazards Program, 69 thunderstorm pentrations were ...
During the Storm Hazards Experiment 1982, the Goddard Space Flight Center monitored radiation from l...
Data waveforms obtained during the 1981 direct strike lightning tests, utilizing the NASA F-106B air...
Tests designed to investigate the lightning-generated electromagnetic environment affecting aircraft...
Data waveforms are presented which were obtained during the 1985 and 1986 direct-strike lightning te...
The triggered lightning environment of the F106B aircraft is investigated. Scale modeling of the F10...
The current knowledge concerning potential lightning effects on aircraft and the means that are avai...
Data waveforms are presented which were obtained during the 1983 direct strike lightning tests utili...
Various characteristics of the electromagnetic data obtained on a NASA F-106B aircraft during direct...