发明名称 Aircraft launched rocket munition has rings behind warhead with reaction drives to correct flight alignment
摘要 The aircraft launched rocket munition (11) has a booster (13) and a ring (16) for flight direction correction. The ring has a miniaturized reaction drive (17) extending radially of the longitudinal axis of the munition, behind the ogival section of the rocket head. There can be multiple rings with reaction drives. The reaction drives can have different power outputs.
申请公布号 DE20221539(U1) 申请公布日期 2006.04.27
申请号 DE2002221539U 申请日期 2002.08.13
申请人 DIEHL BGT DEFENCE GMBH & CO. KG 发明人
分类号 F42B10/60;F42B19/08 主分类号 F42B10/60
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