ESTIMATION OF THE ULTIMATE LANDING SPEEDS TAKING INTO ACCOUNT THE DEGRADATION OF THE STRENGTH CHARACTERISTICS OF PARACHUTE DOME MATERIALS. PART 2. DEPENDENCE OF THE ULTIMATE LANDING SPEEDS ON THE STRENGTH DEGRADATION

Part 2 is a continuation of Part 1 [1], which proposed the dependence of the maximum permissible loads on the parachute on the degradation coefficients of the power structure elements strength characteristics. The condition of equality of safety factors for elements after the long-term operation and...

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Bibliographic Details
Main Author: Петр Александрович Фомичев
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2019-04-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/675