HIGH VISCOSITY THERMAL PROTECTION MATERIALS.
Abstract
A description is given of materials preparation and hot pressing of H-O rocket motor test nozzles of a 31.5% silica-68.5% tungsten composition. It also includes the H-O motor testing of nozzles of similar compositions. Vacuum sintering studies of the material are described in detail.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 13, 1968
- Accession Number
- AD0830801
Entities
People
- Roger E. Wilson
Organizations
- Naval Ordnance Laboratory