Accession Number : AD0439833


Title :   SHOCK TUBE TEST OF A HORN ANTENNA,


Descriptive Note : Technical note.


Corporate Author : BALLISTIC RESEARCH LABS ABERDEEN PROVING GROUND MD


Personal Author(s) : Coulter,George A


Report Date : Oct 1963


Pagination or Media Count : 42


Abstract : The results from air shock loading a model of an inverted horn reflector type antenna are given for incident nominal shock overpressures of 50, 100, and 160 psi. The data are presented in the form of pressure-time traces obtained from piezo-electric transducers flush-mounted at several points on the interior walls of the model. (Author)


Descriptors :   *SHOCK(MECHANICS) , SHOCK(MECHANICS) , HORN ANTENNAS , PRESSURE , PIEZOELECTRIC TRANSDUCERS , SHOCK TUBES , LOADS(FORCES) , INSTRUMENTATION


Distribution Statement : APPROVED FOR PUBLIC RELEASE