ATLAS 'E' SERIES FLY-OUT LAUNCHER STUDY.
Abstract
The report was prepared to document the results of initial studying and testing of an Atlas fly-out launcher system. Specifically the thermodynamic, gas dynamic and acoustical effects on the missile, launcher and launcher equipment were studied to evaluate the system. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1968
- Accession Number
- AD0840804
Entities
Organizations
- General Dynamics