Abstract: An earth coverage antenna system includes a reflector, a feed horn and a strut. The reflector has a circularly symmetric reflector surface. The feed horn is positioned on the symmetry axis of the reflector and is attached to the strut. The feed horn transmits RF microwave energy toward the reflector surface. The antenna system further includes two cables that prevent side-ways movement of the strut. The antenna system further includes a lens assembly that directs microwave energy away from the central region of the reflector. The antenna system further includes a microwave energy scattering device disposed at the center of the reflector to scatter microwave energy away from the feed horn. The reflector surface is defined by a perturbed parabolic geometrical shape that is swept around the symmetry axis. The reflector reflects most microwave energy towards the earth's horizon, but diverts enough microwave energy towards the regions closer to nadir so as to maintain an isoflux of energy on the earth's surface.

Abstract: An antenna system includes a reflector, an offset feed horn and a support platform. The reflector has a reflector surface. The reflector and offset feed horn are attached to the support platform. The offset feed horn transmits RF microwave energy toward the reflector surface. The antenna system further includes a turntable which has a single rotation axis. The turntable rotates about the antenna rotation axis. The support platform is attached to the turntable such that the turntable rotates the support platform. The reflector surface has a perturbed paraboloid geometrical shape that reflects most RF microwave energy along a beam peak pointing direction. The reflector surface reflects RF microwave energy towards the earth's surface in such a manner that the reflected RF microwave energy illuminates a narrow strip of the earth's surface from nadir to a point near the earth's horizon with substantially constant intensity.

Abstract: Various embodiments relate to a low-profile, linearly-polarized patch antenna with parasitic elements at 5.3 GHz for the ISS C-band WiFi band. It may also use the 5.8 GHz band. A protective dome helps to meet low earth orbit space requirements.

Abstract: An antenna system includes a reflector, an offset feed horn and a support platform. The reflector has a reflector surface. The reflector and offset feed horn are attached to the support platform. The offset feed horn transmits RF microwave energy toward the reflector surface. The antenna system further includes a turntable which has a single rotation axis. The turntable rotates about the antenna rotation axis. The support platform is attached to the turntable such that the turntable rotates the support platform. The reflector surface has a perturbed paraboloid geometrical shape that reflects most RF microwave energy along a beam peak pointing direction. The reflector surface reflects RF microwave energy towards the earth's surface in such a manner that the reflected RF microwave energy illuminates a narrow strip of the earth's surface from nadir to a point near the earth's horizon with substantially constant intensity.

Abstract: Various embodiments relate to a low-profile, linearly-polarized patch antenna with parasitic elements at 5.3 GHz for the ISS C-band WiFi band. It may also use the 5.8 GHz band. A protective dome helps to meet low earth orbit space requirements.

Abstract: Various embodiments relate to a low-profile, linearly-polarized patch antenna with parasitic elements at 5.3 GHz for the ISS C-band WiFi band. It may also use the 5.8 GHz band. A protective dome helps to meet low earth orbit space requirements.