F41F 3/055

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9897413 Process for launching a cruise missile from an aircraftJul 22, 16Feb 20, 18Florida Turbine Technologies, Inc.
9163901 Guidance section connector interface for advanced rocket launchersNov 01, 13Oct 20, 15RAYTHEON COMPANY
9091506 Float support member for rocket launcherFeb 27, 13Jul 28, 15AMPHENOL CORPORATION
9074842 Umbilical cable disconnectNov 13, 12Jul 07, 15RAYTHEON COMPANY
8505429 Device for separating the two portions of a launcher refueling moduleMar 30, 10Aug 13, 13SNECMA
7681482 Automatic connector systemSep 03, 08Mar 23, 10THE BOEING COMPANY
7640840 Automated launch mating systemJan 11, 08Jan 05, 10THE BOEING COMPANY
6227117 Retaining device, especially for the rear igniter of a missileOct 13, 98May 08, 01THOMSON-CSF
6152011 System for controlling and independently firing multiple missiles of different typesJan 27, 98Nov 28, 00LOCKHEED MARTIN CORPORATION
5458042 Container for packaging an object provided with a radio frequency transmission device and removable element for such a containerSep 02, 94Oct 17, 95Aerospatiale Societe Nationale Industrielle
5088381 Projectile-launcher actuated by inductionFeb 28, 91Feb 18, 92Thomson-Brandt Armements
4757960 Lost-fluid hydraulic actuation systemMar 27, 86Jul 19, 88CENTRE NATIONAL D'ETUDES SPATIALES
4681017 Practice ammunition systemJul 24, 85Jul 21, 87DYNAMIT NOBEL DEFENCE GMBH