Calculation of protective characteristics of the high-altitude compensating jacket for airplane crews

Aviation technics and technology


Tazetdinov R. G.*, Zotov V. A., Tibirin G. S.**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia



The article is devoted to designing the mathematical model,design procedure and calculation of protective characteristics of a high-altitude compensating jacket (ВКЖ), to protect the pilot from influence of the lowered barometric pressure during high-altitude flight. The methods allow to choose jacket design data at a stage of its designing, reducing thereby number of expensive tests.


high-altitude compensating jacket, booster compensation, power compensation, sealed camera, power shell, tension device, a soft shell of revolution, balance equation, finite difference method

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