An unmanned aerial vehicle (UAV) launch tube that comprises at least one inner layer of prepreg substrate disposed about a right parallelepiped aperture, at least one outer layer of prepreg substrate disposed about the right parallelepiped aperture, and one or more structural panels disposed between the at least one inner layer of prepreg substrate and the at least one outer layer of prepreg substrate. An unmanned aerial vehicle (UAV) launch tube that comprises a tethered sabot configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot is hollow having an open end oriented toward a high pressure volume and a tether attached within a hollow of the sabot and attached to the inner wall retaining the high pressure volume or attach to the inner base wall. A system comprising a communication node and a launcher comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node.

Disclosed is an integrally suppressed barrel which in an embodiment includes a firearm barrel, an outer sleeve, a front end cap, and a plurality of mesh layers. The firearm barrel has at least one set of hole groups to provide venting of propellant gas to a first space between the firearm barrel and the outer sleeve. At least one hole of at least one of the sets of hole groups is sized and threaded to mate with a removable socket head plug and are configurable by the user to vent, or to not vent, based both upon attributes of the ammunition desired for use and upon the desired degree of suppression. The holes of the at least one set of hole groups are elements of an open path for the gas, from behind a fired projectile, to outside the integrally suppressed barrel, as the projectile traverses the bore of the firearm barrel. Movement of the gas vented from forward holes dampens movement of the gas vented from rear holes. The plurality of mesh layers is located in the first space. The plurality of mesh layers disrupts and disperses the wavefront of the gas vented into the first space between the firearm barrel and the outer sleeve. The first space and the plurality of mesh layers are also elements of the open path for the gas. The front end cap threadably coupled to a threaded muzzle end of the firearm barrel applies compression to form a gas-tight seal at both ends of the outer sleeve.

Disclosed is an integrally suppressed barrel which in an embodiment includes a firearm barrel, an outer sleeve, a front end cap, and a plurality of mesh layers. The firearm barrel has at least one set of hole groups to provide venting of propellant gas to a first space between the firearm barrel and the outer sleeve. At least one hole of at least one of the sets of hole groups is sized and threaded to mate with a removable socket head plug and are configurable by the user to vent, or to not vent, based both upon attributes of the ammunition desired for use and upon the desired degree of suppression. The holes of the at least one set of hole groups are elements of an open path for the gas, from behind a fired projectile, to outside the integrally suppressed barrel, as the projectile traverses the bore of the firearm barrel. Movement of the gas vented from forward holes dampens movement of the gas vented from rear holes. The plurality of mesh layers is located in the first space. The plurality of mesh layers disrupts and disperses the wavefront of the gas vented into the first space between the firearm barrel and the outer sleeve. The first space and the plurality of mesh layers are also elements of the open path for the gas. The front end cap threadably coupled to a threaded muzzle end of the firearm barrel applies compression to form a gas-tight seal at both ends of the outer sleeve.

An unmanned aerial vehicle (UAV) launch tube that comprises at least one inner layer of prepreg substrate disposed about a right parallelepiped aperture, at least one outer layer of prepreg substrate disposed about the right parallelepiped aperture, and one or more structural panels disposed between the at least one inner layer of prepreg substrate and the at least one outer layer of prepreg substrate. An unmanned aerial vehicle (UAV) launch tube that comprises a tethered sabot configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot is hollow having an open end oriented toward a high pressure volume and a tether attached within a hollow of the sabot and attached to the inner wall retaining the high pressure volume or attach to the inner base wall. A system comprising a communication node and a launcher comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node.

An unmanned aerial vehicle (UAV) launch tube that comprises at least one inner layer of prepreg substrate disposed about a right parallelepiped aperture, at least one outer layer of prepreg substrate disposed about the right parallelepiped aperture, and one or more structural panels disposed between the at least one inner layer of prepreg substrate and the at least one outer layer of prepreg substrate. An unmanned aerial vehicle (UAV) launch tube that comprises a tethered sabot configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot is hollow having an open end oriented toward a high pressure volume and a tether attached within a hollow of the sabot and attached to the inner wall retaining the high pressure volume or attach to the inner base wall. A system comprising a communication node and a launcher comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node.

A hybrid metal and composite barrel assembly for a firearm preferably includes a metal inner barrel liner and a composite outer barrel sleeve. The composite outer barrel sleeve preferably includes at least one layer of woven metal mesh material comprising a plurality of metallic fibers, and at least one layer of carbon fiber material comprising a plurality of carbon fibers. The composite outer barrel sleeve is preferably engaged around the metal inner barrel liner, and optionally incorporates a tensioning nut to retain the sleeve on the liner.

Methods and systems are provided for a firearms suppressor adapted with blowout panels. In one example, the blowout panels may be configured to have a lower tolerance for pressure than the materials from which outer components of the suppressor are formed. During over pressure events of the suppressor, the blowout panels may rupture, thereby dissipating pressure in the suppressor.

A hybrid composite and steel rifle barrel assembly relating to bolt action rifles or other firearms, including those that fire rimfire or centerfire ammunition. The inner barrel construction consists of a pre-machined and rifled steel barrel that has been machined down from its original geometry to a much lighter and smaller geometry to achieve a significant weight savings. The metal portion of the barrel that is removed, is replaced by a composite tubular structure, that slips over the machined down steel barrel which is then adhesively bonded to the steel barrel. The composite barrel consists of a plurality of concentric composite material layers including carbon fiber-based uni-directional prepreg and a unique metallic weave that is placed within the composite structure to aid in the thermal transfer of heat extending from the chamber to the muzzle end of the rifle barrel. The metallic weave is positioned so that it is the first layer(s) within the composite structure that make direct contact with the steel barrel. This metallic weave is a continuous weave that extends the full length of the barrel and not only provides a highly thermally conductive layer, but also provides significant longitudinal barrel stiffness. The resin matrix system within the composite structure is a standard epoxy resin that preferably does not contain any type of thermally conductive particulate or filler, to achieve an effective thermal transfer layer. The resulting hybrid composite/steel barrel achieves significant weight reduction compared to an all-steel barrel in addition to increased accuracy. In addition to the weight reduction and accuracy benefits associated with this invention, is that the movement of a bullet associated with shooting through a cold barrel (cold bore) versus a hot barrel is reduced substantially.

Provided are methods and related devices for disrupting an explosive device using a propellant driven disrupter (PDD) that propels a rounded projectile (RP) toward an explosive device. The RP travels along a linear trajectory and impacts the target, including a barrier portion of the explosive device. The impacting between the RP and barrier forms a composite projectile via a solid state weld between a portion of the barrier and the RP distal end, thereby minimizing or avoiding spall and fragment generation into the explosive device. The projectile traverses a penetration distance along the linear trajectory, or a defined-angle relative thereto, to disrupt the explosive device without unwanted explosive detonation.

Provided are methods and related devices for disrupting an explosive device using a propellant driven disrupter (PDD) that propels a rounded projectile (RP) toward an explosive device. The RP travels along a linear trajectory and impacts the target, including a barrier portion of the explosive device. The impacting between the RP and barrier forms a composite projectile via a solid state weld between a portion of the barrier and the RP distal end, thereby minimizing or avoiding spall and fragment generation into the explosive device. The projectile traverses a penetration distance along the linear trajectory, or a defined-angle relative thereto, to disrupt the explosive device without unwanted explosive detonation.