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)
Flight Tests Conducted on the Fluidic-Generator System to Environmentally Fire Aircraft Rockets
1970
24 pages
Report
No indication
English
Rockets , Ammunition, Explosives, & Pyrotechnics , Industrial Safety Engineering , Fluid Mechanics , Rocket igniters , Arming devices , Aviation safety , Motor generators , Fluidics , Cavity resonators , Diaphragms(Mechanics) , Coils , Response , Jet plane noise , Rain , Ice , Flight testing , Rocket launchers , Environmental tests , Jet fighters , Naval aircraft , Attack bombers , Silicon controlled rectifiers , Flight decks , A-4 aircraft , A-4e aircraft , F-4 aircraft , Lau-10a launchers , Lau-10 launchers , Zuni
Tema Archive | 2003
|Engineering Index Backfile | 1945
|NTIS | 1981
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