An unmanned aerial vehicle launch tube that has at least one layer of prepeg substrate disposed about an aperture to form a tube, a sabot disposed in an interior of said tube, said sabot having a first clasp tab, and a clasp detachably coupled to said first clasp tab and contacting an inner circumferential wall of said tube so that said clasp is rotationally constrained by the inner circumferential wall and said first clasp tab.
SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE
01.12.2016
Patent
Elektronische Ressource
Englisch
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