Limitations of diluter demand system for oxygen supply at high altitude; limitations of cockpit heating system; problem of forced escape from plane; objections to escape capsule; advantages of ejection seat in fighter aircraft; catapulting of ejection set; defects of transparent plastic enclosures; use of laminated glass; cockpit cooling; instrumentation. (See also Am Soc Mech Engrs -- Advance Paper n 48 -- AV-1 for meeting Sept 20-21 1948 10 p)
Cockpit design problems of high altitude high-speed flight
Mech Eng
Mechanical Engineering ; 70 , n 11
1948
5 pages
Aufsatz (Zeitschrift)
Englisch
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