Aircraft that can operate independently of ground sources of power; self containment for large turbine powered aircraft; obstacles to, and advantages of, self containment; if bleed air from main engines cannot be used for air conditioning because of contamination, independence that self containment offers could be obtained for little or no loss in aircraft performance; system that would satisfy this requirement referred to as basic accessory pneumatic power system.
Self-contained airplane
Aeronautical Eng Rev
Aeronautical Engineering Review ; 13 , n 9
1954
5 pages
Article (Journal)
English
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