System for detachably coupling an unmanned aerial vehicle within a launch tube
An unmanned aerial vehicle launch tube that has 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.
1. A method of launching an unmanned aerial vehicle (UAV) launch, comprising:
generating gas in a gas generator;
introducing said generated gas to a high-pressure volume between an expandable sabot skirt of a sabot and said gas generator to break an adhesive coupling that restrains said sabot in a launch tube, wherein said UAV is on a top surface of said sabot, a bottom of said sabot opposite to said top surface is open ended, and said expandable sabot skirt is a portion of a side surface of said sabot disposed proximate said open ended bottom of said sabot;
pushing said expandable sabot skirt against an inner circumferential wall of said launch tube using said generated gas; and
driving said sabot up said launch tube using said generated gas.
2. The method of claim 1 , wherein said adhesive coupling comprises an adhesive coupling between said expandable skirt and a shell surrounding said gas generator.
3. The method of claim 1 , further comprising:
clasping a UAV to said sabot using a clasp; and
restraining said clasp against said inner circumferential wall of said launch tube to prevent said clasp from decoupling from at least one of: said UAV and said sabot.
4. The method of claim 3 , further comprising:
sliding said clasp past said inner circumferential wall to release said clasp from at least one of: said UAV and said sabot.
5. The method of claim 3 , further comprising:
tethering said sabot to said launch tube to prevent said sabot from exiting said launch tube.
6. A method of launching an unmanned aerial vehicle (UAV) launch, comprising:
restraining a sabot in a launch tube;
introducing gas to a high-pressure side of an expandable sabot skirt of a sabot to break said restraint of said sabot in said launch tube, wherein said UAV is on a top surface of said sabot, a bottom of said sabot opposite to said top surface is open ended, and said expandable sabot skirt is a portion of a side surface of said sabot disposed proximate said open ended bottom of said sabot; and
driving said sabot up said launch tube using said gas.
7. The method of claim 6 , further comprising:
pushing said expandable sabot skirt against an inner circumferential wall of said launch tube using said gas.
8. The method of claim 7 , wherein said restraining a sabot comprises restraining said sabot using an adhesive.
9. The method of claim 8 , wherein said restraining said sabot using an adhesive further comprises restraining an expandable skirt of said sabot to a shell surrounding a gas generator in said launch tube.
10. The method of claim 9 , further comprising:
tethering said sabot to said launch tube.
11. The method of claim 6 , wherein said expandable sabot skirt further comprises a circumferential skirt protrusion that extends from said expandable sabot skirt toward an inner circumferential wall of said launch tube.
12. The method of claim 6 , further comprising:
restraining the travel of said sabot by a tether configured to prevent said sabot from exiting said launch tube, and wherein the restrained travel of said sabot substantially retains said gas within said launch tube.
13. The method of claim 12 wherein said tether is attached to said sabot and said inner circumferential wall of said launch tube by at least one of: a tether reel and a winding element.