发明名称 DEVICE FOR SEPARATION AND JETTISON OF PAYLOAD FAIRING OF CARRIER MISSILE
摘要 FIELD: armaments and ammunition.SUBSTANCE: invention can be used to separate and to jettison the payload fairing of the carrier missile. The device for separation and jettison of payload fairing of carrier missile with possibility of rotation, pushers supported by the carrier missile fittings, shank with spherical end edges, springs with opposite direction of winding, and installed one in another. The pusher contains telescopically connected with each other external cylinder with sleeve with rigidly connected bottom lid with small sleeve, and internal cylinder with rod with rigidly secured top lid with sleeve. The sleeves are telescopically connected with each other with cavity creation between the bottom and top lids.EFFECT: invention improves reliability of separation and jettison of the payload fairing.2 dwg
申请公布号 RU2568965(C1) 申请公布日期 2015.11.20
申请号 RU20140142344 申请日期 2014.10.22
申请人 AKTSIONERNOE OBSHCHESTVO "VOENNO-PROMYSHLENNAJA KORPORATSIJA "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE MASHINOSTROENIJA" (AO "VPK "NPO MASHINOSTROENIJA") 发明人 SHESTAKOV SERGEJ ALEKSANDROVICH;ZEMSKOV VJACHESLAV ALEKSANDROVICH;GORJAEV ANDREJ NIKOLAEVICH
分类号 B64G1/64;F42B15/36 主分类号 B64G1/64
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