Patent classifications
H01Q15/162
Antenna
An antenna having a reflector mounted on a rigid boom uses a line feed or phased array feed to operate in the Ka band with frequencies up to 36 gigahertz while maintaining the ability to operate at frequencies down to L-Band of 1-2 GHz.
Antenna
An antenna having a reflector mounted on a rigid boom uses a line feed or phased array feed to operate in the Ka band with frequencies up to 36 gigahertz while maintaining the ability to operate at frequencies down to L-Band of 1-2 GHz.
Radome, reflector, and feed assemblies for microwave antennas
A microwave antenna includes an antenna housing and a radome fabric attached to the housing, which is configured to pass microwave electromagnetic signals therethrough. The radome fabric has an opening formed therein. A vent component is attached to the radome fabric so as to cover the opening in the radome fabric when the radome fabric is viewed from an elevation view in a direction parallel to an axis extending through and perpendicular to the opening in the radome fabric. The vent component is configured to allow air to pass between the atmosphere and the antenna housing.
Quad band petal reflector antenna
The present invention provides a petal reflector antenna that comprises a main reflector having a paraboloid shape and a plurality of identical petals, a feed assembly that includes a horn, a wideband junction, a holder, and a hybrid coupler connected to a diplexer and a multiplexer. The petal reflector antenna further comprises a protective radome cover, a horn, a subreflector, and a support station member for quickly and conveniently set up over a desired ground location. The petal reflector antenna can operate simultaneously in the K, Ka, Ku receive, and Ku transmit frequency bands.
Deployable Membrane Structure for an Antenna
A deployable membrane structure for an antenna comprises a membrane comprising a plurality of first regions of higher-stiffness material integrally connected via one or more second regions of lower-stiffness material, wherein the one or more second regions are formed from compliant material configured to permit the membrane to be folded into a collapsed configuration and subsequently unfolded into a deployed configuration, and are arranged so as to allow adjacent ones of the plurality of first regions to be folded so as to lie against one another. In some embodiments the membrane is formed of a composite material comprising a plurality of fibres in a compliant matrix, and the plurality of first regions comprise material with a higher fibre density than the one or more second regions. A deployable antenna comprising the deployable membrane structure is also disclosed.
2.2M Offset Antenna
A 2.2M offset antenna includes a reflector hub; a positioner for supporting the reflector hub; a plurality of reflector panels including a first plurality of side panels and a second plurality of side panels, the first plurality of side panels and the second plurality of side panels each being selectively securable to the reflector hub; each side panel of the first plurality of side panels being uniquely sized relative to the other side panels of the first plurality of side panels such that the first plurality of side panels may be nested together in a stacked configuration when separated from reflector hub; and each side panel of the second plurality of side panels being uniquely sized relative to the other side panels of the second plurality of side panels such that the second plurality of side panels may be nested together in a stacked configuration when separated from reflector hub.
MESH REFLECTOR SATELLITE ANTENNAS WITH ON-ORBIT EXTRUDED OR PRINTED SUPPORT STRUCTURE
Deployable reflector antenna includes a fabrication hub in which at least one additive fabrication unit disposed. The additive fabrication unit is configured to form at least one rigid structural element of a reflector antenna system. In a stowed condition, an RF reflector material comprised of a flexible webbing is disposed in a stowed configuration proximate to the fabrication hub. A fabrication control system controls the additive fabrication unit so as to form the at least one rigid structural element. The RF reflector material is arranged to transition during the additive fabrication process from the stowed configuration in which the flexible webbing material is furled compactly at the fabrication hub, to a deployed configuration in which the flexible webbing material is unfurled.
Antenna
An antenna having a reflector mounted on a rigid boom uses a line feed or phased array feed to operate in the Ka band with frequencies up to 36 gigahertz while maintaining the ability to operate at frequencies down to L-Band of 1-2 GHz.
Mesh reflector satellites antennas with on-orbit extruded or printed supported structure
Deployable reflector antenna includes a fabrication hub in which at least one additive fabrication unit disposed. The additive fabrication unit is configured to form at least one rigid structural element of a reflector antenna system. In a stowed condition, an RF reflector material comprised of a flexible webbing is disposed in a stowed configuration proximate to the fabrication hub. A fabrication control system controls the additive fabrication unit so as to form the at least one rigid structural element. The RF reflector material is arranged to transition during the additive fabrication process from the stowed configuration in which the flexible webbing material is furled compactly at the fabrication hub, to a deployed configuration in which the flexible webbing material is unfurled.
Mesh antenna reflector with deployable perimeter
Antenna reflector has a reflector surface which forms a predetermined dish-like shape. The reflector surface includes an inner section which radially extends a first predetermined distance from a main dish axis. This inner section is immovably supported on a fixed backing structure. The reflector surface also includes an outer section comprising a deployable perimeter. A deployable support structure is comprised of a plurality of rib tips hingedly secured to the fixed backing structure, each having an elongated shape, and extending in a direction away from the main dish axis. The rib tips are configured to rotate on hinge members relative to the fixed backing structure from a first position in which the reflector antenna is made more compact for stowage, to a second position in which a diameter of the reflector surface is increased at a time of deployment.