Heat-loaded trajectory selection for durability valuation of aviation guided missile airframe

Аuthors

Volkov V. N.^*, Gusev A. N.^**, Ivakha V. V.

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

*e-mail: ivakha@mail.ru
**e-mail: kaf701mai@mail.ru

Abstract

The article devoted to heat-loaded trajectory selection for durability valuation and ground-based test execution of aviation guided missile load-bearing unit elements. The introduced approach allows selecting material of aviation guided missile load-bearing unit elements with durability assurance in all service conditions at projecting phase.

Keywords:

aviation guided missile, trajectory, load factor, safety factor, stability factor, airframe, propulsion system