COMPATIBILITY OF ELASTOMERS WITH LIQUID PROPELLANTS. AN ANNOTATED BIBLIOGRAPHY
Abstract
Fifty-two references are presented on the effects of liquid rocket propellants on elastomeric materials. The propellants investigated include inhibited red fuming nitric acid, nitrogen tetraoxide oxide, nitrogen oxide, unsymmetrical dimethylhydrazine, and hydrazine. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1962
- Accession Number
- AD0275279
Entities
People
- William A. Hollister
Organizations
- Lockheed Martin Missiles and Space