Effects of Proof Testing and Temperature/Humidity on a Candidate Viper Motor Case Material
Abstract
This report presents the results of an in-house investigation of the effect of proof testing and subsequent exposure to an accelerated aging environment of 140 deg F and 95% relative humidity for one particular fiberglass epoxy system.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 21, 1977
- Accession Number
- ADA042576
Entities
People
- J. B. Cobb
- O. C. Fuchtnicht
- R. J. Thompson
Organizations
- United States Army Aviation and Missile Command