Shock Testing of a Kulite Pressure Gage
Abstract
A program designed to measure in-flight base pressure is presently underway at the Launch and Flight Division of the Ballistic Research Laboratory. The pressure gages used in the projectile must withstand projectile accelerations (from 10,000-20,000 g's) if they are to be effective. Shock tests were performed on Kulite pressure gages model No. XT-39-190-25A to determine its response to this type of acceleration level. This report details the workings of the Impac Shock Machine as well as the effect of acceleration on gage performance.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1991
- Accession Number
- ADA243962
Entities
People
- James M. Garner
- Timothy J. Mcaveney
Organizations
- Ballistic Research Laboratory