发明名称 |
MISSILE PART WITH STABILISER OF ROCKET PROJECTILE |
摘要 |
FIELD: weapons and ammunition.SUBSTANCE: missile part with stabiliser of rocket projectile comprises a housing with the multinozzle unit and a foldout stabiliser with blades. The blades are mounted at a zero angle to the longitudinal axis of the housing. The stabiliser blades are made flat and have an asymmetrical tapering of chamfered front edges. The chamfer is located on the surface of the blade facing in the direction opposite to the rotation of the missile part. The angle of tapering in a plane perpendicular to the front edges is located within ?=10°-30°.EFFECT: increase reliability of functioning of the missile part.3 cl, 2 dwg |
申请公布号 |
RU2540291(C1) |
申请公布日期 |
2015.02.10 |
申请号 |
RU20140111566 |
申请日期 |
2014.03.27 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "SPLAV" |
发明人 |
MAKAROVETS NIKOLAJ ALEKSANDROVICH;ALJAZHEDINOV VADIM RASHITOVICH;TREGUBOV VIKTOR IVANOVICH;VERBOVENKO ALEKSANDR ANDREEVICH;KASHIRKIN ALEKSANDR ALEKSANDROVICH;BAZARNYJ ALEKSEJ NIKOLAEVICH;EROKHIN VLADIMIR EVGEN'EVICH;ZAKHAROV SERGEJ OLEGOVICH |
分类号 |
F42B15/00;F42B15/01 |
主分类号 |
F42B15/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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