An antenna array has wideband high gain characteristics and includes: a dielectric; a loop provided on a first surface of the dielectric and that has a first slot and a second slot; a first feed pin provided at a position corresponding to the first slot on a second surface of the dielectric; a second feed pin provided at a position corresponding to the second slot on the second surface of the dielectric; and a divider provided between the first feed pin and the second feed pin, and electrically connected to the loop.

Examples disclosed herein relate to an Insulated Glass Unit (“IGU”) to enhance wireless communications in a wireless network. The IGU has a first and a second glass layers, a first and a second spacers, and a first and a second ground planes, the first ground plane in contact with the first glass layer and the second ground plane in contact with the second glass layer. The IGU also includes a gas layer in between the first and the second ground planes, a reflectarray comprising a metastructure array of reflector elements, and a third glass layer on top of the metastructure reflectarray.

A system may include a meta-surface including multiple unit cells arranged along the meta-surface. Structural parameters of each unit cell may vary along the meta-surface. The system may further include at least a first active feed unit directed toward the meta-surface to generate a first beam. The first active feed unit may be configured to move relative to the meta-surface parallel to a 2-dimensional plane. The first beam is steerable by moving the first active feed unit.

A satellite system can include one or more satellites that orbit the Earth. The one or more satellites may have satellite buses that support antenna arrays. The antenna arrays may include space fed arrays. Each space fed array may have an antenna feed array and an inner array that is coupled to a direct radiating array. The direct radiating array may operate in the same satellite band as the space fed array, or upconversion and downconversion circuitry may be used to communicatively couple a direct radiating array that operates in a different satellite band to the space fed array. The satellites may have peripheral walls with corner fittings that can be selected to provide the satellite bus with particular leg strengths. This can reduce overall mass of the satellites in a payload fairing while accommodating different types of antenna arrays.

An antenna apparatus includes a ground layer, patch antenna patterns, feed vias, ring-type meta patterns, and coupling-type meta patterns. The ground layer has one or more through-holes. Patch antenna patterns are each disposed above the ground layer. Feed vias are disposed to penetrate through the one or more through-holes, and electrically connect to the patch antenna patterns, respectively. Ring-type meta patterns are arranged between the patch antenna patterns. Coupling-type meta patterns are alternately arranged between the patch antenna patterns in fewer numbers than the ring-type meta patterns in positions more distant from the patch antenna patterns than positions in which the ring-type meta patterns are arranged.

A wave shaping device which comprises a tunable impedance surface and a controller connected to the surface in order to control its impedance. The shaping device further comprises a transmission module for receiving a pilot signal used to control the impedance of the surface.

A wave shaping device which comprises a tunable impedance surface and a controller connected to the surface in order to control its impedance. The shaping device further comprises a transmission module for receiving a pilot signal used to control the impedance of the surface.

A satellite system can include one or more satellites that orbit the Earth. The one or more satellites may have satellite buses that support antenna arrays. The antenna arrays may include space fed arrays. Each space fed array may have an antenna feed array and an inner array that is coupled to a direct radiating array. The direct radiating array may operate in the same satellite band as the space fed array, or upconversion and downconversion circuitry may be used to communicatively couple a direct radiating array that operates in a different satellite band to the space fed array. The satellites may have peripheral walls with corner fittings that can be selected to provide the satellite bus with particular leg strengths. This can reduce overall mass of the satellites in a payload fairing while accommodating different types of antenna arrays.

Examples disclosed herein relate to an Insulated Glass Unit (“IGU”) to enhance wireless communications in a wireless network. The IGU has a first and a second glass layers, a first and a second spacers, and a first and a second ground planes, the first ground plane in contact with the first glass layer and the second ground plane in contact with the second glass layer. The IGU also includes a gas layer in between the first and the second ground planes, a reflectarray comprising a metastructure array of reflector elements, and a third glass layer on top of the metastructure reflectarray.

Directive gain antenna elements implemented with an aperture-fed patch array antenna assembly are described. A feed network for the aperture-fed patch array may include offset apertures and may also include meandering feed lines. Scalable aperture shapes and orientations that can be used with antennas operating at any frequency and with dual orthogonal polarizations are also disclosed. Directive gain antenna elements implemented with arrays of orthogonal reflected dipoles are also described with optimal feed networks and parasitic elements to achieve desired directive gain characteristics. Such arrayed dipole antennas feature dual orthogonal polarizations with assembly tabs that lower cost and improve reliability. Backhaul radios that incorporate said antennas are also disclosed.