Single event effect hardness for the front-end ASICs in the DAMPE satellite BGO calorimeter
The Dark Matter Particle Explorer (DAMPE) is a Chinese scientific satellite designed for cosmic ray studies with a primary scientific goal of indirect detection of dark matter particles. As a crucial sub-detector, the BGO calorimeter measures the energy spectrum of cosmic rays in the energy range fr...
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Veröffentlicht in: | Chinese physics C 2016, Vol.40 (1), p.86-91 |
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description | The Dark Matter Particle Explorer (DAMPE) is a Chinese scientific satellite designed for cosmic ray studies with a primary scientific goal of indirect detection of dark matter particles. As a crucial sub-detector, the BGO calorimeter measures the energy spectrum of cosmic rays in the energy range from 5 GeV to 10 TeV. In order to implement high-density front-end electronics (FEE) with the ability to measure 1848 signals from 616 photomultiplier tubes on the strictly constrained satellite platform, two kinds of 32-channel front-end ASICs, VA160 and VATA160, are customized. However, a space mission period of more than 3 years makes single event effects (SEEs) become threats to reliability. In order to evaluate SEE sensitivities of these chips and verify the effectiveness of mitigation methods, a series of laser-induced and heavy ion-induced SEE tests were performed. Benefiting from the single event latch-up (SEL) protection circuit for power supply, the triple module redundancy (TMR) technology for the configuration registers and the optimized sequential design for the data acquisition process, 52 VA160 chips and 32 VATA160 chips have been applied in the flight model of the BGO calorimeter with radiation hardness assurance. |
doi_str_mv | 10.1088/1674-1137/40/1/016102 |
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Benefiting from the single event latch-up (SEL) protection circuit for power supply, the triple module redundancy (TMR) technology for the configuration registers and the optimized sequential design for the data acquisition process, 52 VA160 chips and 32 VATA160 chips have been applied in the flight model of the BGO calorimeter with radiation hardness assurance.</description><identifier>ISSN: 1674-1137</identifier><identifier>EISSN: 0254-3052</identifier><identifier>DOI: 10.1088/1674-1137/40/1/016102</identifier><language>eng</language><subject>ASIC ; BGO ; BGO (crystal) ; Chips (electronics) ; Cosmic rays ; Dark matter ; Electronics ; Satellites ; Single Event Effects ; Space telescopes ; 前端电子学 ; 单粒子效应 ; 卫星设计 ; 硬度 ; 量热计 ; 阻尼</subject><ispartof>Chinese physics C, 2016, Vol.40 (1), p.86-91</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c313t-4091864aba5d70df0c9d228636a9314a113931b1c15cc785f640a730a4b78fbb3</citedby><cites>FETCH-LOGICAL-c313t-4091864aba5d70df0c9d228636a9314a113931b1c15cc785f640a730a4b78fbb3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://image.cqvip.com/vip1000/qk/92043A/92043A.jpg</thumbnail><link.rule.ids>314,776,780,4010,27900,27901,27902</link.rule.ids></links><search><creatorcontrib>高山山 蒋荻 封常青 习凯 刘树彬 安琪</creatorcontrib><title>Single event effect hardness for the front-end ASICs in the DAMPE satellite BGO calorimeter</title><title>Chinese physics C</title><addtitle>Chinese Physica C</addtitle><description>The Dark Matter Particle Explorer (DAMPE) is a Chinese scientific satellite designed for cosmic ray studies with a primary scientific goal of indirect detection of dark matter particles. 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Benefiting from the single event latch-up (SEL) protection circuit for power supply, the triple module redundancy (TMR) technology for the configuration registers and the optimized sequential design for the data acquisition process, 52 VA160 chips and 32 VATA160 chips have been applied in the flight model of the BGO calorimeter with radiation hardness assurance.</description><subject>ASIC</subject><subject>BGO</subject><subject>BGO (crystal)</subject><subject>Chips (electronics)</subject><subject>Cosmic rays</subject><subject>Dark matter</subject><subject>Electronics</subject><subject>Satellites</subject><subject>Single Event Effects</subject><subject>Space telescopes</subject><subject>前端电子学</subject><subject>单粒子效应</subject><subject>卫星设计</subject><subject>硬度</subject><subject>量热计</subject><subject>阻尼</subject><issn>1674-1137</issn><issn>0254-3052</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNo9kE1LAzEYhIMoWKs_QQievKybbD42PdZaa6FSoXryELLZpF3ZZtskFfz3Zq30vQwMMy_DA8AtRg8YCZFjXtIMY1LmFOU4R5hjVJyBASoYzQhixTkYnDKX4CqEL4Q4TdUB-Fw1bt0aaL6Ni9BYa3SEG-VrZ0KAtvMwbgy0vnMxM66G49V8EmDj_uyn8evbFAYVTds20cDH2RJq1Xa-2Zpo_DW4sKoN5uZfh-Djefo-eckWy9l8Ml5kmmASM4pGWHCqKsXqEtUW6VFdFIITrkYEU5VWJ62wxkzrUjCbpquSIEWrUtiqIkNwf_y7893-YEKU2ybotEk50x2CxCKBYJhRnqLsGNW-C8EbK3dprPI_EiPZw5Q9KNmDkjQ58ggz9e7-e5vOrfeJ2anIeclEf-QXKqZxAg</recordid><startdate>2016</startdate><enddate>2016</enddate><creator>高山山 蒋荻 封常青 习凯 刘树彬 安琪</creator><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>~WA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7U5</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>2016</creationdate><title>Single event effect hardness for the front-end ASICs in the DAMPE satellite BGO calorimeter</title><author>高山山 蒋荻 封常青 习凯 刘树彬 安琪</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c313t-4091864aba5d70df0c9d228636a9314a113931b1c15cc785f640a730a4b78fbb3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>ASIC</topic><topic>BGO</topic><topic>BGO (crystal)</topic><topic>Chips (electronics)</topic><topic>Cosmic rays</topic><topic>Dark matter</topic><topic>Electronics</topic><topic>Satellites</topic><topic>Single Event Effects</topic><topic>Space telescopes</topic><topic>前端电子学</topic><topic>单粒子效应</topic><topic>卫星设计</topic><topic>硬度</topic><topic>量热计</topic><topic>阻尼</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>高山山 蒋荻 封常青 习凯 刘树彬 安琪</creatorcontrib><collection>中文科技期刊数据库</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>CrossRef</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Chinese physics C</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>高山山 蒋荻 封常青 习凯 刘树彬 安琪</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Single event effect hardness for the front-end ASICs in the DAMPE satellite BGO calorimeter</atitle><jtitle>Chinese physics C</jtitle><addtitle>Chinese Physica C</addtitle><date>2016</date><risdate>2016</risdate><volume>40</volume><issue>1</issue><spage>86</spage><epage>91</epage><pages>86-91</pages><issn>1674-1137</issn><eissn>0254-3052</eissn><abstract>The Dark Matter Particle Explorer (DAMPE) is a Chinese scientific satellite designed for cosmic ray studies with a primary scientific goal of indirect detection of dark matter particles. As a crucial sub-detector, the BGO calorimeter measures the energy spectrum of cosmic rays in the energy range from 5 GeV to 10 TeV. In order to implement high-density front-end electronics (FEE) with the ability to measure 1848 signals from 616 photomultiplier tubes on the strictly constrained satellite platform, two kinds of 32-channel front-end ASICs, VA160 and VATA160, are customized. However, a space mission period of more than 3 years makes single event effects (SEEs) become threats to reliability. In order to evaluate SEE sensitivities of these chips and verify the effectiveness of mitigation methods, a series of laser-induced and heavy ion-induced SEE tests were performed. Benefiting from the single event latch-up (SEL) protection circuit for power supply, the triple module redundancy (TMR) technology for the configuration registers and the optimized sequential design for the data acquisition process, 52 VA160 chips and 32 VATA160 chips have been applied in the flight model of the BGO calorimeter with radiation hardness assurance.</abstract><doi>10.1088/1674-1137/40/1/016102</doi><tpages>6</tpages></addata></record> |
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subjects | ASIC BGO BGO (crystal) Chips (electronics) Cosmic rays Dark matter Electronics Satellites Single Event Effects Space telescopes 前端电子学 单粒子效应 卫星设计 硬度 量热计 阻尼 |
title | Single event effect hardness for the front-end ASICs in the DAMPE satellite BGO calorimeter |
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