Antenna and RF system for fly-away satellite terminal communication applications on Ka-band
ABSTRACT Antenna and RF system for fly‐away satellite terminal communication applications on ka‐band is presented in this article. Fly‐away satellite terminals 1 or 2 people is fixed by installing motion terminal, movement and installation of equipment, and ease of operation to the user's for l...
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Veröffentlicht in: | Microwave and optical technology letters 2016-08, Vol.58 (8), p.2020-2025 |
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creator | Park, Byung Jun Kim, Chun Won Lee, Deok Woo Lee, Sung Jae |
description | ABSTRACT
Antenna and RF system for fly‐away satellite terminal communication applications on ka‐band is presented in this article. Fly‐away satellite terminals 1 or 2 people is fixed by installing motion terminal, movement and installation of equipment, and ease of operation to the user's for low‐power consumption, small size, and light weight is important. For low‐power consumption and compact and light‐weight, dual‐reflector antenna system volume using dual‐offset Gregorian antenna structure is minimized, magnesium by weight is minimized. Transmitter part of RF systems has low‐power consumption and compact light weight using the pHEMT MMIC compound devices. For harmonic rejection, the photonic band‐gap low‐pass‐filter is designed. In receiver part, low‐noise amplifier and down converter rolled into one function of the low‐noise block converter structure is designed for compact and light weight. In this article, fly‐away satellite terminal with low‐power consumption and compact light weight is described by antenna system and RF system performances. © 2016 Wiley Periodicals, Inc. Microwave Opt Technol Lett 58:2020–2025, 2016 |
doi_str_mv | 10.1002/mop.29960 |
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Antenna and RF system for fly‐away satellite terminal communication applications on ka‐band is presented in this article. Fly‐away satellite terminals 1 or 2 people is fixed by installing motion terminal, movement and installation of equipment, and ease of operation to the user's for low‐power consumption, small size, and light weight is important. For low‐power consumption and compact and light‐weight, dual‐reflector antenna system volume using dual‐offset Gregorian antenna structure is minimized, magnesium by weight is minimized. Transmitter part of RF systems has low‐power consumption and compact light weight using the pHEMT MMIC compound devices. For harmonic rejection, the photonic band‐gap low‐pass‐filter is designed. In receiver part, low‐noise amplifier and down converter rolled into one function of the low‐noise block converter structure is designed for compact and light weight. In this article, fly‐away satellite terminal with low‐power consumption and compact light weight is described by antenna system and RF system performances. © 2016 Wiley Periodicals, Inc. Microwave Opt Technol Lett 58:2020–2025, 2016</description><identifier>ISSN: 0895-2477</identifier><identifier>EISSN: 1098-2760</identifier><identifier>DOI: 10.1002/mop.29960</identifier><identifier>CODEN: MOTLEO</identifier><language>eng</language><publisher>New York: Blackwell Publishing Ltd</publisher><subject>antenna and RF system ; Antennas ; Communication satellites ; Communication systems ; Consumption ; dual-offset Gregorian ; fly-away satellite terminal ; photonic band-gap-low-pass-filter ; Radio frequencies ; Satellites ; Terminals ; Weight reduction</subject><ispartof>Microwave and optical technology letters, 2016-08, Vol.58 (8), p.2020-2025</ispartof><rights>2016 Wiley Periodicals, Inc.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c3680-fa5c49d62c7aeba24773b3335ccfdc793c65eedc2622c621f3e186589a66ae523</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1002%2Fmop.29960$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1002%2Fmop.29960$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,780,784,1416,27923,27924,45573,45574</link.rule.ids></links><search><creatorcontrib>Park, Byung Jun</creatorcontrib><creatorcontrib>Kim, Chun Won</creatorcontrib><creatorcontrib>Lee, Deok Woo</creatorcontrib><creatorcontrib>Lee, Sung Jae</creatorcontrib><title>Antenna and RF system for fly-away satellite terminal communication applications on Ka-band</title><title>Microwave and optical technology letters</title><addtitle>Microw. Opt. Technol. Lett</addtitle><description>ABSTRACT
Antenna and RF system for fly‐away satellite terminal communication applications on ka‐band is presented in this article. Fly‐away satellite terminals 1 or 2 people is fixed by installing motion terminal, movement and installation of equipment, and ease of operation to the user's for low‐power consumption, small size, and light weight is important. For low‐power consumption and compact and light‐weight, dual‐reflector antenna system volume using dual‐offset Gregorian antenna structure is minimized, magnesium by weight is minimized. Transmitter part of RF systems has low‐power consumption and compact light weight using the pHEMT MMIC compound devices. For harmonic rejection, the photonic band‐gap low‐pass‐filter is designed. In receiver part, low‐noise amplifier and down converter rolled into one function of the low‐noise block converter structure is designed for compact and light weight. In this article, fly‐away satellite terminal with low‐power consumption and compact light weight is described by antenna system and RF system performances. © 2016 Wiley Periodicals, Inc. Microwave Opt Technol Lett 58:2020–2025, 2016</description><subject>antenna and RF system</subject><subject>Antennas</subject><subject>Communication satellites</subject><subject>Communication systems</subject><subject>Consumption</subject><subject>dual-offset Gregorian</subject><subject>fly-away satellite terminal</subject><subject>photonic band-gap-low-pass-filter</subject><subject>Radio frequencies</subject><subject>Satellites</subject><subject>Terminals</subject><subject>Weight reduction</subject><issn>0895-2477</issn><issn>1098-2760</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNp1kEtPwzAQhC0EEuVx4B9Y4gKHFD8SOz5WFQVEoQgVOHCwtq4jBfLCTgT597gEOCBx2l3pm9HsIHREyZgSws7KuhkzpQTZQiNKVBoxKcg2GpFUJRGLpdxFe96_EEK4lGyEnidVa6sKMFRrfD_DvvetLXFWO5wVfQTv0GMPrS2KvLW4ta7MKyiwqcuyq3IDbV5XGJqm-N49Dvc1RKvgd4B2Mii8Pfye--hhdr6cXkbzxcXVdDKPDBcpiTJITKzWghkJdgWbkHzFOU-MydZGKm5EYu3aMMGYEYxm3NJUJKkCIcAmjO-jk8G3cfVbZ32ry9ybEBkqW3de05QlsaSKbdDjP-hL3bnwUaCkoqniNI0DdTpQxtXeO5vpxuUluF5Tojc161Cz_qo5sGcD-54Xtv8f1DeLux9FNCjyUPXHrwLcqxaSy0Q_3V7op8flo5jPlvqOfwIFJo47</recordid><startdate>201608</startdate><enddate>201608</enddate><creator>Park, Byung Jun</creator><creator>Kim, Chun Won</creator><creator>Lee, Deok Woo</creator><creator>Lee, Sung Jae</creator><general>Blackwell Publishing Ltd</general><general>Wiley Subscription Services, Inc</general><scope>BSCLL</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>L7M</scope><scope>7QF</scope><scope>JG9</scope></search><sort><creationdate>201608</creationdate><title>Antenna and RF system for fly-away satellite terminal communication applications on Ka-band</title><author>Park, Byung Jun ; Kim, Chun Won ; Lee, Deok Woo ; Lee, Sung Jae</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3680-fa5c49d62c7aeba24773b3335ccfdc793c65eedc2622c621f3e186589a66ae523</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>antenna and RF system</topic><topic>Antennas</topic><topic>Communication satellites</topic><topic>Communication systems</topic><topic>Consumption</topic><topic>dual-offset Gregorian</topic><topic>fly-away satellite terminal</topic><topic>photonic band-gap-low-pass-filter</topic><topic>Radio frequencies</topic><topic>Satellites</topic><topic>Terminals</topic><topic>Weight reduction</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Park, Byung Jun</creatorcontrib><creatorcontrib>Kim, Chun Won</creatorcontrib><creatorcontrib>Lee, Deok Woo</creatorcontrib><creatorcontrib>Lee, Sung Jae</creatorcontrib><collection>Istex</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Aluminium Industry Abstracts</collection><collection>Materials Research Database</collection><jtitle>Microwave and optical technology letters</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Park, Byung Jun</au><au>Kim, Chun Won</au><au>Lee, Deok Woo</au><au>Lee, Sung Jae</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Antenna and RF system for fly-away satellite terminal communication applications on Ka-band</atitle><jtitle>Microwave and optical technology letters</jtitle><addtitle>Microw. Opt. Technol. Lett</addtitle><date>2016-08</date><risdate>2016</risdate><volume>58</volume><issue>8</issue><spage>2020</spage><epage>2025</epage><pages>2020-2025</pages><issn>0895-2477</issn><eissn>1098-2760</eissn><coden>MOTLEO</coden><abstract>ABSTRACT
Antenna and RF system for fly‐away satellite terminal communication applications on ka‐band is presented in this article. Fly‐away satellite terminals 1 or 2 people is fixed by installing motion terminal, movement and installation of equipment, and ease of operation to the user's for low‐power consumption, small size, and light weight is important. For low‐power consumption and compact and light‐weight, dual‐reflector antenna system volume using dual‐offset Gregorian antenna structure is minimized, magnesium by weight is minimized. Transmitter part of RF systems has low‐power consumption and compact light weight using the pHEMT MMIC compound devices. For harmonic rejection, the photonic band‐gap low‐pass‐filter is designed. In receiver part, low‐noise amplifier and down converter rolled into one function of the low‐noise block converter structure is designed for compact and light weight. In this article, fly‐away satellite terminal with low‐power consumption and compact light weight is described by antenna system and RF system performances. © 2016 Wiley Periodicals, Inc. Microwave Opt Technol Lett 58:2020–2025, 2016</abstract><cop>New York</cop><pub>Blackwell Publishing Ltd</pub><doi>10.1002/mop.29960</doi><tpages>6</tpages></addata></record> |
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subjects | antenna and RF system Antennas Communication satellites Communication systems Consumption dual-offset Gregorian fly-away satellite terminal photonic band-gap-low-pass-filter Radio frequencies Satellites Terminals Weight reduction |
title | Antenna and RF system for fly-away satellite terminal communication applications on Ka-band |
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