A razor wire rapid deployment unit (RDU)/barrier is disclosed. In some embodiments, the RDU includes an enclosure having a first section coupleable with a second section, the enclosure defining an interior area therein. The RDU may further include a razor wire disposed within the interior area of the enclosure, a first end of the razor wire directly coupled to the first section, and a second end of the razor wire directly coupled to the second section. The first and second sides of the enclosure may be separated from one another to deploy the razor wire from a compressed configuration to an expanded configuration.

A razor wire rapid deployment unit (RDU)/barrier is disclosed. In some embodiments, the RDU includes an enclosure having a first section coupleable with a second section, the enclosure defining an interior area therein. The RDU may further include a razor wire disposed within the interior area of the enclosure, a first end of the razor wire directly coupled to the first section, and a second end of the razor wire directly coupled to the second section. The first and second sides of the enclosure may be separated from one another to deploy the razor wire from a compressed configuration to an expanded configuration.

A system and method that uses one or more jet engines to remove unmanned aircraft from restricted airspace. Generally, the force created by a jet engine can be used to remove drones or other unwanted objects from the restricted airspace. Once the system determines the presence of an unauthorized aircraft or object within the restricted airspace, the jet engine(s) can be activated and used to pull the drone or flying object towards the jet engine though the force created by the intake of the jet engine(s), or to expel the drone or object from the restricted area through the force created by the exhaust of the jet engine(s).

A system and method that uses one or more jet engines to remove unmanned aircraft from restricted airspace. Generally, the force created by a jet engine can be used to remove drones or other unwanted objects from the restricted airspace. Once the system determines the presence of an unauthorized aircraft or object within the restricted airspace, the jet engine(s) can be activated and used to pull the drone or flying object towards the jet engine though the force created by the intake of the jet engine(s), or to expel the drone or object from the restricted area through the force created by the exhaust of the jet engine(s).

A ballistic-resistant barrier assembly including an elongated barrier having a vertical portion including a substantially horizontal elongated top edge, and a ballistic-resistant device having a first ballistic-resistant panel including an elongated top edge, and an engagement portion affixed to the elongated top edge of the first ballistic-resistant panel, wherein the engagement portion of the ballistic-resistant device is disposed adjacent the elongated top edge of the barrier so that the first ballistic-resistant panel is disposed in a vertical orientation adjacent the vertical portion of the barrier.

A protective barrier system designed to protect against high-energy events, such as impacts from ballistic threats or blasts. In one embodiment, the protective barrier system comprises a blast mitigation panel in the front (on the threat side of the barrier), a ballistic resistant panel in the back (on the asset side of the barrier), and a frame that is configured to incorporate the blast mitigation panel and ballistic resistant panel, and stand the panels upright so as to form a barrier. The blast mitigation panel and ballistic resistant panel are modular and are easily attached to and detached from the frame to create a protective barrier that can be easily customized to protect structures or assets of nearly any shape or size from both blasts and ballistics. For example, another embodiment is a protective barrier system that may be used as body armor or personal protection for an individual.

A protective barrier system designed to protect against high-energy events, such as impacts from ballistic threats or blasts. In one embodiment, the protective barrier system comprises a blast mitigation panel in the front (on the threat side of the barrier), a ballistic resistant panel in the back (on the asset side of the barrier), and a frame that is configured to incorporate the blast mitigation panel and ballistic resistant panel, and stand the panels upright so as to form a barrier. The blast mitigation panel and ballistic resistant panel are modular and are easily attached to and detached from the frame to create a protective barrier that can be easily customized to protect structures or assets of nearly any shape or size from both blasts and ballistics. For example, another embodiment is a protective barrier system that may be used as body armor or personal protection for an individual.

A razor wire barrier is disclosed. In some embodiments, an enclosure includes a plurality of panel sections rotatably coupled together, at least one panel section of the plurality of panel sections including a first frame component directly coupled to a second frame component of an adjacent panel section. The enclosure may further include a razor wire panel extending across each of plurality of panel sections.

A razor wire barrier is disclosed. In some embodiments, an enclosure includes a plurality of panel sections rotatably coupled together, at least one panel section of the plurality of panel sections including a first frame component directly coupled to a second frame component of an adjacent panel section. The enclosure may further include a razor wire panel extending across each of plurality of panel sections.

A razor wire rapid deployment unit (RDU)/barrier is disclosed. In some embodiments, the RDU includes an enclosure having a first section coupleable with a second section, the enclosure defining an interior area therein. The RDU may further include a razor wire disposed within the interior area of the enclosure, a first end of the razor wire directly coupled to the first section, and a second end of the razor wire directly coupled to the second section. The first and second sides of the enclosure may be separated from one another to deploy the razor wire from a compressed configuration to an expanded configuration.