HYPERSONIC FIRINGS OF A SPHERE-CONE CONFIGURATION.
Abstract
Drag and stability coefficients were obtained from free-flight model firings in the 1,000-ft. Hyperballistics Range No. 4. All tests were conducted at a Mach number of 12. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 15, 1965
- Accession Number
- AD0369024
Entities
People
- Jeanne B. Jusino
Organizations
- Naval Ordnance Laboratory