Shaped beam horn antenna for enhanced gain at edge of global coverage
Ramesh Chandra Gupta, Milind Bhagwan Rao Mahajan, Rajeev Jyoti
Abstract
Ramesh Chandra Gupta, Milind Bhagwan Rao Mahajan, Rajeev Jyoti
Abstract
This paper reports design and development of a new shaped beam horn antenna for enhanced gain at edge of global coverage. The horn is designed at Ku-band (10.7–11.2 GHz). This horn is tailored for specific shaped beam for global coverage. It has three sections: stepped section, axial corrugated section and radial corrugated section. Shaped beam is achieved with help of multi-modes at aperture of the horn. The horn is analysed and optimised using Mode-Matching-Technique- and Method-of-Moments-based software TICRA CHAMP. It is fabricated with aluminium alloy 6061T6 material using computerised-numerically-controlled-based turning machine. The measured return loss and patterns match well with predicted one. The fabricated shaped global horn has established measured return loss >17 dB, cross-polarisation discrimination (<−40 dB) and enhanced edge of coverage gain (>18.36 dB). The methodology of horn design offers extra degree of flexibility to design a variety of shaped horn antennas with tailored radio frequency performances for specific spacecraft application.
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This paper reports design and development of a new shaped beam horn antenna for enhanced gain at edge of global coverage. The horn is designed at Ku-band (10.7–11.2 GHz). This horn is tailored for specific shaped beam for global coverage. It has three sections: stepped section, axial corrugated section and radial corrugated section. Shaped beam is achieved with help of multi-modes at aperture of the horn. The horn is analysed and optimised using Mode-Matching-Technique- and Method-of-Moments-based software TICRA CHAMP. It is fabricated with aluminium alloy 6061T6 material using computerised-numerically-controlled-based turning machine. The measured return loss and patterns match well with predicted one. The fabricated shaped global horn has established measured return loss >17 dB, cross-polarisation discrimination (<−40 dB) and enhanced edge of coverage gain (>18.36 dB). The methodology of horn design offers extra degree of flexibility to design a variety of shaped horn antennas with tailored radio frequency performances for specific spacecraft application.
Key concepts: French horn, Horn antenna, Return loss, Antenna gain, Feed horn, Aperture (computer memory), Antenna (radio), Enhanced Data Rates for GSM Evolution