• Title/Summary/Keyword: 안테나 햇(antenna hat)

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아리랑 위성 2호 X-대역 안테나 햇 제작 및 시험

  • Lee, Jin-Ho;Lee, Na-Young;Moon, Hong-Youl;Kim, Hee-Seob;Kim, Gyu-Sun
    • Aerospace Engineering and Technology
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    • v.4 no.1
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    • pp.103-107
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    • 2005
  • There is an X-band transmission system in KOMPSAT-2 in order to downlink the acquired image data in high speed. KOMPSAT-2 employs a steerable high gain X-band antenna for that purpose. During the ground test, the X-band RF radiation is so strong that it has to be controlled for safety, while spacecraft needs to keep flight configuration. Also in a launch site of which all test facilities are the subjects of strict radiation control, the antenna system should be tested again without any change in the configuration. To limit the actual radiation of RF power, an antenna hat was manufactured and thoroughly tested to demonstrate the spacecraft safety when using it.

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Compact S-Band Antenna Hat for RF Compatibility Testing of Launch Vehicle (발사체의 RF 호환성 시험을 위한 소형 S-밴드 안테나 햇)

  • Kim, Sung-Wan;Park, Dong-Chul
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.26 no.2
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    • pp.148-157
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    • 2015
  • In this paper, we propose a compact antenna hat to perform RF compatibility testing efficiently between the launch vehicle and ground stations. The proposed structure implements a small size and low loss using the conductive shield instead of the conventional RF absorber. The S-band antenna hat, which is fabricated for an inverted-F onboard antenna with the size of $74mm{\times}13mm{\times}16mm$, has the small enclosure of $88mm{\times}35mm{\times}44mm$, the return loss of 25.6 dB, the insertion loss of 0.26 dB, and the leakage loss of 49.4 dB at the center frequency of 2.25 GHz. The simulated and measured results show a good agreement.

KOMPSAT-2 Payload Downlink System Verification (아리랑 위성 2호 탑재체 하향링크 시스템 검증)

  • Lee, Jin-Ho;Kim, Hui-Seop;Cheon, Yong-Sik
    • Aerospace Engineering and Technology
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    • v.5 no.2
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    • pp.108-113
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    • 2006
  • This paper includes the test results of KOMPSAT-2 payload downlink system which were measured for the purpose of performance verification. The antenna beam patterns which indicates the status of the interface & antenna itself, were measured as well as the antenna VSWR. The checkout of the transponder & its spectrum was followed and this made sure that there was no spurious output distinguished. Finally a test for BER verification was conducted between satellite and receiving system for their compatibility through the antenna-to-antenna connection using an antenna hat. Verification tests for an RF system should be performed after relocation, integration and test for environments in order to make sure that no degradation happens.

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