FIELD: engines and pumps.
SUBSTANCE: invention relates to countermeasures against guided missiles including the application of heat trap. Proposed method is based on detection of guided missile with thermal homing head. It consists in determination of aircraft current speed for adjustment of thrust and actuation of heat trap jet engine. Blow-out charge is fired along with heat trap thermal substance, heat trap is ejected and its flight is stabilised in required direction. Then, heat trap jet engine is switched on to drive the trap by engine thrust at required speed.
EFFECT: increased range of heat trap flight.
2 dwg
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