METHOD OF TEST OF ROCKET FAIRINGS OF NONMETALLIC MATERIALS Russian patent published in 2017 - IPC G01N3/18 

FIELD: testing equipment.

SUBSTANCE: carry out force to the exterior surface of the fairing via multilayer structure consisting of a rigid shell, elastic fluid, flexible and discrete heat insulation and contact the heater, and external components strength loads are applied to the outer surface of the rigid shell. The transverse force is applied in the plane perpendicular to the longitudinal force application plane, and the thermal insulation consists of discrete sectors of the equidistant outer surface of the fairing. In the plane of application of longitudinal forces on the external surface of the fairing, a flexible thermal insulation is mounted through the heater.

EFFECT: increasing the accuracy of reproduction of the power load on the rocket fairing and increasing the technical capabilities of equipment for ground testing of new designs of missile technology.

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