High Viscosity Thermal Protection Materials.
Abstract
Initial objectives of this work were to develop a high temperature resistant material capable of withstanding rocket nozzle throat, leading edge, or re-entry environments by virtue of its high temperature strength, resistance to oxidation, and ability to cool itself ablatively. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 25, 1969
- Accession Number
- AD0851223
Entities
People
- F. J. Koubek
- Roger E. Wilson
Organizations
- Naval Ordnance Laboratory