Predicting Peak Pressure Levels of Shoulder-Launched Rockets and Missiles.
Abstract
Based on impulse noise measurements at the gunner position for various proposed and developed shoulder-launched rockets and missiles, a simple relationship was formulated to forecast peak pressure levels of future systems as a function of concept parameters. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1977
- Accession Number
- ADA041333
Entities
People
- Georges R. Garinther
- Gerald Chaikin
Organizations
- Human Engineering Laboratory