发明名称 REACTION NOZZLE WITH ADJUSTABLE ALTITUDE TOLERANCE
摘要 FIELD: rocketry. ^ SUBSTANCE: in proposed reaction nozzle with adjustable altitude tolerance provided with one or several ring slots in supersonic part overlapped by sector gates hinge-mounted over perimeter of nozzle before each slot, said slots are formed by one or several heads rigidly connected to each other and connected to nozzle, and said sector gates are hinge-connected on outer surfaces of nozzle heads and are provided with their turning mechanisms. ^ EFFECT: improved reliability of control mechanism of reaction nozzle altitude characteristics. ^ 3 cl, 1 dwg
申请公布号 RU2322607(C2) 申请公布日期 2008.04.20
申请号 RU20040117948 申请日期 2004.06.16
申请人 OAO "NPO EHNERGOMASH IM. AKAD. V.P. GLUSHKO" 发明人 SERGIENKO ALEKSANDR ALEKSANDROVICH;SEMENOV VASILIJ VASIL'EVICH;CHVANOV VLADIMIR KONSTANTINOVICH;CHEL'KIS FELIKS JUR'EVICH;FEDOROV VLADIMIR VLADIMIROVICH
分类号 F02G1/00;F02K9/97 主分类号 F02G1/00
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