Dual reflector antenna
Abstract
Abstract An earth station antenna is employed for telecommunicating with a satellite in combination with an automatic tracking apparatus. The antenna is a dual reflector antenna which comprises a main reflector, a sub-reflector and a primary radiator, and the used frequency band of the antenna is at least 1.8 octaves. A parameter t of the antenna, defined by a configuration of the primary radiator is less than 0.3 at the lowest operating frequency. The phase center of the primary radiator, at a low frequency within the operating frequency range, is made to correspond with the focus of the sub-reflector. The above parameter t is defined by: ##EQU1## where: λ: wavelength in free space, D h : aperture diameter of the primary radiator, L h : center axial length from the radiator apex to the radiator aperture plane, and L s : length from the radiator aperture plane to the bottom surface of the sub-reflector.
Inventors
- 👤 Takashi Katagi
- 👤 Shuji Urasaki
- 👤 Takashi Ebisui
- 👤 Katsuhiko Aoki
Bibliographic Details
Claims Analysis
Total Claims: 5References Cited (Backward Citations)
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