FIELD: weapons.
SUBSTANCE: invention is related to design of targets intended for operation with radiolocating and thermal armament systems. Aviation target comprises body with cover, head part, torch in the form of cylinder with fuel composition and bottom, parachute system comprising braking and main canopies, disengaging mechanism. The main canopy comprises corner reflector and is installed in chamber packed in case that is rigidly connected to bottom of torch and split-disengaging mechanism. Braking canopy is located in case, which is rigidly connected to body cover. Dead eye of the main canopy via cable is connected to torch bottom, and dead eye of braking canopy is connected as a whole with disengaging mechanism and chamber of the main canopy.
EFFECT: increased efficiency of target action due to increase of specific efficiency and reliability of action with simultaneous expansion of production resources in its manufacture.
5 cl, 5 dwg
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Authors
Dates
2009-05-10—Published
2007-10-17—Filed