发明名称 Canard-type guided missile - has stabiliser at rear end with appreciably less wing span than canard surfaces preceding it
摘要 <p>The missile has one or more canard surfaces for control purposes. There is a stabiliser or tailplane installed aft of the canard surfaces. The wingspan of the stabiliser is appreciably less than that of the canard surfaces. The design allows light-weight and low resistance to be combined with great ease of control. The stabiliser surfaces are fixed, while the canard surfaces move for control by direct lift and change of attitude.</p>
申请公布号 DE3047389(A1) 申请公布日期 1981.09.17
申请号 DE19803047389 申请日期 1980.12.16
申请人 MOTOROLA,INC. 发明人 H. RAPP,GIRARD
分类号 F42B10/64;(IPC1-7):42B15/16 主分类号 F42B10/64
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