Abstract: An apparatus and method for mounting a reflector antenna system on an outer surface of an aircraft which minimizes a swept arc of a main reflector. This allows the effective frontal area of the main reflector to be reduced such that a radome with a smaller frontal area can be employed to cover the antenna system. The preferred embodiments make use of a platform which rotates the main reflector about an azimuthal axis which is disposed forwardly of an axial center of the main reflector. In one embodiment, the azimuthal axis is located in a plane extending between the outermost lateral edges of the main reflector. In another embodiment the azimuthal axis is located forwardly of the outermost lateral edges of the main reflector.

Abstract: A reflector for use under a radome disposed on a mobile platform such as an aircraft for reflecting a portion of the electromagnetic energy radiated by an antenna disposed under the radome such that the reflected portion of energy impinges the radome at an angle normal thereto, thereby reducing or eliminating further reflections of the reflected portion of energy within the radome toward the mobile platform on which the radome is mounted. In one preferred embodiment the radome includes a base portion which is covered with a cover of radar absorbing material (RAM). In another embodiment the radome includes a curved base portion which is adapted to match the curvature of the surface of the mobile platform on which the reflector is mounted.

Abstract: A reflector antenna system having a diplexer for providing isolation between transmitted and received signals, which eliminates the need for a diplexer to be inserted into the waveguide or coax transmission line coupling the antenna system with an external antenna electronics subsystem. The antenna system includes a main reflector to which is coupled a low effective dielectric tube. Transmit and receive feedhorns are supported within the tube. A hyperboloidal receive bandpass filter is supported in front of the receive feedhorn and a hyperboloidal transmit bandpass filter is disposed in front of the transmit feedhorn. The receive bandpass filter allows the received signal to pass therethrough but blocks the transmitted signal from the transmit feedhorn. Conversely, the transmit bandpass filter reflects the received signal received from the subreflector surface back towards the receive feedhorn while allowing the transmitted signal from the transmit feedhorn to pass therethrough.

Abstract: A fairing for use with a phased array antenna for attenuating the transverse magnetic (TM) electric field radiated by the antenna, to thereby reduce the possibility of interference with other transceivers operating in the area of the antenna but which are not the intended recipients of a signal transmitted by the antenna. The fairing is adapted to be secured to an outer surface of a fuselage of an aircraft and to support the phased array antenna thereon. The fairing includes a plurality of concentrically arranged channels that serve to capture and ground the TM electric field as it propagates along the plane of the fairing away from the phased array antenna. Advantageously, the phased array antenna is mounted on the fairing so that the fairing also acts as a heat sink to help cool the antenna. In one preferred form the fairing is made from aluminum.