Test Report, HAWK Launcher Shock Absorber Spring, Part Number 9089062, Spring Rate and Residual Deflection Tests.
Abstract
This report presents a description of the tests performed to determine the spring dimensional and load/compression characteristics of the Hawk launcher shock absorber spring and their results. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 26, 1981
- Accession Number
- ADA105804
Entities
People
- John D. Alston
Organizations
- United States Army Aviation and Missile Command