FIELD: test equipment.
SUBSTANCE: invention relates to aircraft-rocket test equipment, namely to testing method for strength under effect of vibration of aircraft guided missiles assembled in laboratory bench conditions. Tests are carried out on three mutually perpendicular axes. During testing, the equipment is rigidly fixed to the table of vibration exciters by means of a device which ensures absence of resonances in a given excitation frequency range. Levels of side lateral vibrations during tests are minimum relative to the specified one.
EFFECT: technical result consists in maximum approximation of independent tests of equipment on vibration loads at test bench to standard suspension conditions under aircraft carrier.
7 cl, 2 dwg
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