Eighteen missiles of various configurations have been flight tested, and all of the components and systems have performed correctly. The major accomplishments of this program have been: 1) the proven capability of the design team to develop and flight test a complete fluidic control system in a reasonable schedule and for a reasonable cost, and 2) the proven repeatability, reliability, and ruggedness of the fluidics components during the experimental programs.
Fluidics in missile control systems
Fluidik in Flugkoerper-Regelungssystemen
Fluidics Quarterly ; 6 , 3 ; 31-42
1974
Aufsatz (Zeitschrift)
Englisch
SAE Technical Papers | 1967
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SAE Technical Papers | 1967
|“FLUIDICS - POTENTIAL FOR REMOTE CONTROL APPLICATIONS”
SAE Technical Papers | 1967
|Emerald Group Publishing | 1967
|Hydraulic fluidics stabilizes helicopter
Engineering Index Backfile | 1968
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