A strapping device for binding an object which has a cross section having a regular-shaped perimeter, the device includes a strap having a clamping strip which forms a loop intended to surround the object, the clamping strip has a central part which has a shape essentially following the shape of the perimeter of the cross section of the object and two strip strands having the respective ends of the clamping strip, the shape of which departs from the shape of the perimeter of the cross section of the object, the strap having at least one so-called central shoe which is mounted on at least one of the strip strands in such a way as to be designed to be interposed between the object and the strip strand.

The system for a collapsible direction finding antenna. The antenna comprising a rigid central portion and a plurality of foldable arms. The antenna is aerial/kite lifted once launched from a tube to provide increased line of sight above a surface. The antennas being launchable from a UUV, a user in the field, and the like. The antenna being a full azimuth direction finding antenna. In some cases, operating at a wide matched frequency of 1 to 6 GHz.

The system for a collapsible direction finding antenna. The antenna comprising a rigid central portion and a plurality of foldable arms. The antenna is aerial/kite lifted once launched from a tube to provide increased line of sight above a surface. The antennas being launchable from a UUV, a user in the field, and the like. The antenna being a full azimuth direction finding antenna. In some cases, operating at a wide matched frequency of 1 to 6 GHz.

A strapping device for binding an object which has a cross section having a regular-shaped perimeter, the device includes a strap comprising a clamping strip which forms a loop intended to surround the object, the clamping strip comprising a central part which has a shape essentially following the shape of the perimeter of the cross section of the object and two strip strands comprising the respective ends of the clamping strip, the shape of which departs from the shape of the perimeter of the cross section of the object, the strap comprising at least one so-called central shoe which is mounted on at least one of the strip strands in such a way as to be designed to be interposed between the object and the strip strand.

A strapping device for binding an object which has a cross section having a regular-shaped perimeter, the device includes a strap comprising a clamping strip which forms a loop intended to surround the object, the clamping strip comprising a central part which has a shape essentially following the shape of the perimeter of the cross section of the object and two strip strands comprising the respective ends of the clamping strip, the shape of which departs from the shape of the perimeter of the cross section of the object, the strap comprising at least one so-called central shoe which is mounted on at least one of the strip strands in such a way as to be designed to be interposed between the object and the strip strand.

A multi-function radio frequency (MFRF) system may deploy groups of small or micro-sized unmanned aircraft systems (UAS) to achieve various MFRF functions and mission objectives. Each member UAS may incorporate structurally integrated/embedded, conformal/appliqu, or mechanically deployable antenna elements, or may utilize characteristic mode transducers to excite conductive exterior surfaces of the UAS, such that each UAS may maximize its limited size or surface area to emit MFRF radiation according to a variety of MFRF operating modes. Member UAS may be fashioned by three-dimensional additive manufacturing (3DAM) techniques. Each UAS may coordinate their positioning and MFRF emissions with other member UAS to collectively form synthetic apertures and swarms capable of MFRF functionalities not achievable by a single UAS. UAS swarms may form new subswarms or dynamically reconfigure depending on changing mission objectives or battlefield conditions.

An antenna structure includes a metallic member, a feed portion, and a coupling resistor. The metallic member defines a slot, a first gap, a second gap, and a third gap. The first gap and the second gap are connected with the slot and divide with the slot the metallic member into a first portion and a second portion. The second portion is grounded. The third gap is defined on the first portion and connected with the slot. The first portion is divided into a radiating portion and a coupling portion by the third gap. The coupling portion is spaced apart from the radiating portion. The feed portion is electrically connected to the radiating portion, and the coupling portion is grounded through the coupling resistor.

The present disclosure provides systems and methods associated with an antenna system comprising a tension member configured to be towed by an aerial platform. In some embodiments, a first end of the tension member may be secured to the aerial platform and the second end may extend unsecured from the aerial platform at a different elevation than the first end. A plurality of antenna assemblies, each comprising at least one antenna, may be secured to and spaced along the length of the tension member. Each of the plurality of antennas may be adapted for use with a particular frequency or frequency bandwidth. For example, each of the plurality of antennas may be adapted or tuned for one or more frequencies useful for synthetic aperture radar (SAR). In some embodiments, a receiving system, a communication link, and/or an antenna location system may be utilized.

The present disclosure provides systems and methods associated with an antenna system comprising a tension member configured to be towed by an aerial platform. In some embodiments, a first end of the tension member may be secured to the aerial platform and the second end may extend unsecured from the aerial platform at a different elevation than the first end. A plurality of antenna assemblies, each comprising at least one antenna, may be secured to and spaced along the length of the tension member. Each of the plurality of antennas may be adapted for use with a particular frequency or frequency bandwidth. For example, each of the plurality of antennas may be adapted or tuned for one or more frequencies useful for synthetic aperture radar (SAR). In some embodiments, a receiving system, a communication link, and/or an antenna location system may be utilized.

An aerial deployed radio antenna system includes a primary aerial vehicle and a plurality of secondary aerial vehicles coupled to the primary aerial vehicle with a primary tether, wherein the plurality of secondary aerial vehicles are coupled to each other with a plurality of secondary tethers. The system also includes a radar-reflective sheet suspended between and supported by a plurality of cables coupled to the plurality of secondary aerial vehicles, wherein the radar-reflective sheet forms a parabolic reflector shape when deployed and towed by the primary aerial vehicle. A radar transmitter/receiver is positioned relative to the radar-reflective sheet to transmit radar signals toward the radar-reflective sheet and receive radar signals focused by the radar-reflective sheet, and a plurality of solar cells is positioned on the radar-reflective sheet. The plurality of solar cells are electrically coupled to a power collector configured to supply solar-generated electrical power to the radar transmitter/receiver.