Aeroballistic MODEL FOR TEST erosive action

摘要

Utility model "aeroballistic model for testing erosive effect" refers to the test equipment or devices of different designs and is intended for land-dynamic testing of structural materials of aircraft and missiles at the erosive effect of atmospheric formations (rain, snow, hail, dust). The purpose of the utility model is to provide aeroballistic model providing its movement in the erosion zone atmospheric formations with a constant prescribed rate and to minimize the contact surface of the test material samples retarding material catcher. The problem is solved as follows: persistence airspeed model zone erosive effects of atmospheric formations provided solid fuel rocket motor mounted in the tail part aeroballistic model while minimizing the contact surface of the test material samples retarding separator material provided opening during flight brake flaps model aeroballistic lead to a reversal in the direction of flight model 180 °, i.e. "Tail" forward, and the input model in the trap of its tail.