Abstract: An elliptical portion having planform cross-section involving a generally circular configuration and an elevational cross-section having at least a partial elliptical configuration; a conical portion having at least one of a conical configuration and a frustoconical configuration, the conical portion coupled with the elliptical portion; and a modifier feed, the modifier feed having a first feed element and a second feed element, whereby the antenna apparatus is configured to perform as a monopole antenna at a low frequency and as a hybrid monopole-biconical antenna at a high frequency.

Abstract: An apparatus includes first and second antenna elements each having a tapered width end, with the tapered width ends being separated by a gap. A portion of the edge of the tapered width end of the each antenna element has a thickness less than a thickness of the remainder of the respective antenna element. Such portion may be the portion of the edge of the antenna elements closest to a feed point of the antenna elements, and may be angled to a point or a flat edge. The thickness of the tapered width ends increases along the width and/or the height of the respective antenna element as the antenna element extends from the feed point.

Abstract: A system may include a base portion, first and second support members coupled to the base portion, a first plurality of tapered slot antenna (TSA) pairs coupled to the first support member, and a second plurality of TSA pairs coupled to the second support member. The first plurality TSA pairs are oriented at a non-zero angle about a first axis of the first support member and are oriented at a non-zero angle about a second axis of the first support member, with the second axis being perpendicular to the first axis. The second plurality TSA pairs are oriented at a non-zero angle about a first axis of the second support member and are oriented at a non-zero angle about a second axis of the second support member, with the second axis being perpendicular to the first axis.

Abstract: A system may include a base portion, first and second support members coupled to the base portion, a first plurality of tapered slot antenna (TSA) pairs coupled to the first support member, and a second plurality of TSA pairs coupled to the second support member. The first plurality TSA pairs are oriented at a non-zero angle about a first axis of the first support member and are oriented at a non-zero angle about a second axis of the first support member, with the second axis being perpendicular to the first axis. The second plurality TSA pairs are oriented at a non-zero angle about a first axis of the second support member and are oriented at a non-zero angle about a second axis of the second support member, with the second axis being perpendicular to the first axis.

Abstract: A spiral antenna apparatus utilizes a noise suppression sheet that is interposed between the spiral antenna element and its ground plane. The noise suppression sheet permits an extremely compact spiral antenna apparatus while lessening antenna performance degradation.

Abstract: A system and method are provided for conditioning a received signal prior to transmission. The signal is separated into different signal components in respective contiguous frequency channels. Each signal component is routed through either time domain or frequency domain processing circuitry and simultaneously a sample of the signal component is routed through control signal generation circuitry. The time domain processing circuitry contains a delay such that if any portion of the signal component exceeds a reference voltage signal, a switch is opened using a control signal generated by the control signal generation circuitry to blank that portion of the signal for that particular frequency channel. The outputs of each frequency channel are then combined into an output signal for transmission. A processor may be used to automatically configure various components within the time domain and frequency domain processing circuitry to prevent excessive power signals from being transmitted.

Abstract: A compact, broadband, aerodynamically streamlined, mechanically rugged antenna for aircraft and other applications has been developed that has a VSWR of 2:1 or better, and has uniform patterns with no nulls over a wide 8:1 bandwidth from 225 MHz to 1.85 GHz. The antenna has an aerodynamically streamlined shape, with a rugged housing capable of withstanding velocities up to Mach 2. In addition to its usage on aircraft, this antenna would be useful in a wide range of applications as a general purpose, wide bandwidth omnidirectional antenna. The antenna achieves its performance capabilities with the use of a double Vivaldi element feed section, an upper extension made of resistive film or R-card, and a shaped boundary between the feed and upper sections of the radiating elements.

Abstract: A compact, omnidirectional, broadband biconical antenna is described, having a first segment with its tip coincident with a horizontal plane, with an elevation angle between 23 degrees and 30 degrees from the horizontal plane; an open second segment joined to a distal end of the first segment, an elevation angle approximately 30 degrees greater than the first segment angle; an open third segment joined to a distal end of the open second segment, an elevation angle approximately 30 degrees greater than the open second segment angle; an open fourth resistive film segment joined to a distal end of the open third segment, an elevation angle approximately equal to the open third segment angle, wherein the segments are mirrored to form a biconical antenna; and a transmission line coupled to the tip of the first segment, interior to the first segment.

Abstract: An antenna includes a support structure and radiating element. The radiating element includes a dielectric planar substrate having a first and a second surface, at least two conductive spiral arms extending outward from and spiraling about an axis of rotation formed on the first surface, and a feed conductor extending outward from and spiraling about an axis of rotation formed on the second surface. The feed conductor may be substantially aligned with one of the conductive spiral arms. When the support structure is placed upon a substantially planar surface, the radiating element is positioned at height h from the planar surface, wherein height h is about one-fourth the wavelength of the antenna's operating frequency. The antenna may produce an omni-directional antenna pattern in azimuth and a broad antenna pattern in elevation, with both patterns having nulls near the horizon. An external reflector may be operatively coupled to the antenna.

Abstract: A concave tapered slot antenna. The antenna includes a first antenna element, a second antenna element and a concave dielectric lens. The first and second antenna elements are situated in a tapered slot antenna configuration. The concave dielectric lens is situated between said first and second antenna elements so that a 3 dB beamwidth for selected frequencies is increased. A method for fabricating concave tapered slot antennas is also described.