Flight Tests Conducted on the Fluidic-Generator System to Environmentally Fire Aircraft Rockets,
Abstract
This report contains a description, results and conclusions of flight tests conducted on a fluidic-generator system to environmentally control the firing of aircraft rockets. A spurious-noise acoustic test conducted on the fluidic-generator system is also discussed. Test results are considered successful. Also included are graphs, illustrations of components, and testing configurations. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 13, 1970
- Accession Number
- AD0872393
Entities
People
- Clayton D. Mckindra
Organizations
- Naval Ordnance Laboratory