发明名称 AIRCRAFT FLARE WARHEAD
摘要 FIELD: military equipment, in particular non-guided aircraft flares intended for illumination of terrain at night. SUBSTANCE: flare warhead 1 has tail section 2, gas-discharge tube 3, illuminating compound 4 and nose section 5 for accommodation of the parachute system and additional burster charge. The warhead is connected to engine 6 by means of fastening member 7, whose cavity 8 accommodates fuze 9. Fuze body 10 accommodates safety-and-actuating mechanism 11 and burster charge 12 which may be positioned both before and behind of mechanism 11. Body 10 is furnished with holes 13 and 14, has shoulder 17 and is connected to tube 3 by means of threaded calibrated connection 18. Engine 6 is thread-joined to fastening member 7. At operation of the device charge 12 is inflamed, then the additional burster charge of the parachute system, the parachute system is actuated, the illuminating compound is inflamed, and flare warhead 1 is separated from the engine. EFFECT: enhanced efficiency due to reduction of passive mass. 2 dwgi
申请公布号 RU2103652(C1) 申请公布日期 1998.01.27
申请号 SU19863144543 申请日期 1986.06.03
申请人 INSTITUT PRIKLADNOJ FIZIKI 发明人 BELIKOV L.V.;KRAVCHENKO A.A.;BELIKOV L.V.;KRAVCHENKO A.A.
分类号 F42B12/42;(IPC1-7):F42B12/42 主分类号 F42B12/42
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