A test technique was developed for applying a full scale mean value (30 kiloampere peak) simulated lightning return stroke current on a complete flight ready aircraft to assess the threat of lightning to aircraft electrical circuits. A computer-aided generator design was used to establish the parameters of the test system. Data from previous work done on development of low inductance current paths determined the basic system configuration.
Full scale lightning test technique
1980-04-01
Conference paper
No indication
English
Full scale lightning generation techniques for aircraft susceptibility evaluations
Tema Archive | 1997
|Simulated Lightning Test Shuttle .03 Scale Model
NTIS | 1974
|Simulated lightning test shuttle .03 scale model
NTRS | 1974
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