Review of jet hydraulic system data indicated that two-thirds of all hydraulic system incidents during past 2 yr have been due to external system leakage in areas of lines, fittings, hoses, and seals; these areas must be given extensive consideration in design of SST; preliminary studies indicate that approximately 700 hydraulic hp may be used for various hydraulic systems; this might include 250 hp for flight control system; it is anticipated that hydraulic system operational temperatures will vary from 350 to 500 F.
Supersonic transport aircraft hydraulic systems
J Aircraft
Journal of Aircraft ; 1 , n 1
1964
7 pages
Article (Journal)
English
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SUPERSONIC TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
AIAA | 1963
|Supersonic transport aircraft hydraulic systems
AIAA | 1964
|Emerald Group Publishing | 1961
Engineering Index Backfile | 1962
|Engineering Index Backfile | 1961