发明名称 Launcher rail for missiles
摘要 The launcher rail for missiles consists of an elongated, rectangular housing having a profiled rail which has an interior which is open at one end (on one side). Two guide grooves in which adjustable-height profiled strips are arranged are provided on the two outer longitudinal sides of the rail. In addition, two longitudinal grooves are provided in the interior for the accommodation of an adaptor rail whose interior is matched to a sliding element of another missile which is to be launched. <IMAGE>
申请公布号 DE4321379(A1) 申请公布日期 1995.01.05
申请号 DE19934321379 申请日期 1993.06.26
申请人 DEUTSCHE AEROSPACE AG, 80804 MUENCHEN, DE 发明人 BARTL, JOSEF, 85110 KIPFENBERG, DE;FISCHER, MANFRED, 85521 OTTOBRUNN, DE;KERLE, NORBERT, 85604 ZORNEDING, DE
分类号 B64D1/06;F41F3/04;(IPC1-7):F41F7/00 主分类号 B64D1/06
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