SHOCK TUBE TEST OF A HORN ANTENNA,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1963
- Accession Number
- AD0439833
Entities
People
- George A. Coulter
Organizations
- Ballistic Research Laboratory