DEVELOPMENT OF HIGH-STRENGTH IMPREGNATED ROVING FOR FILAMENT WINDING.
Abstract
This is the fourth of a series of bimonthly reports describing progress in a program conducted to improve uniformity and strength utilization in preimpregnated roving for filamentwound rocket chambers. The work, is being conducted. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 20, 1964
- Accession Number
- AD0435034
Entities
Organizations
- Aerojet Rocketdyne Holdings