A CONTROL ACTUATION ASSEMBLY FOR A MINIATURE, GUIDED MISSILE

The present invention relates to a control actuation assembly for a miniature, guided missile comprising a seat (20) having a support plate (22) that is transversally mounted to an inner chamber limited by a hollow, elongated main body (10); and at least one wing pair (40) having first and second ae...

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Bibliographische Detailangaben
Hauptverfasser:	SİLİK, Yusuf, TANIKER, Semih, GÜNGÖR, Mahmut Emre
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AMMUNITION AVIATION BLASTING COSMONAUTICS EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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