Rocket Motor Blast Effects and Proposed Ablative Protection for Ram Launching System EX 43. Addendum.
Abstract
The results of the flyaway and environmental tests of ablative materials described in this report show that (1) all of the materials tested are satisfactory for use in the RAM launching system and (2) Dow Corning 93-104 w/graphite is an acceptable adhesive for bonding of the recommended materials to the launcher and/or deck surface.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1980
- Accession Number
- ADA083315
Entities
People
- Allen B. Coates
- Earl E. Biermann
Organizations
- Naval Surface Warfare Center Dahlgren Division