Predicting the effect of radiation damage on dark current in a space-qualified high performance CMOS image sensor
The CIS115 is a Teledyne-e2v CMOS image sensor with 1504×2000 pixels of 7 μm pitch. It has a high optical quantum efficiency owing to a multi-layer anti-reflective coating and its backside illuminated construction, and low dark current due to its pinned photodiode 4T pixel architecture. The sensor o...
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Veröffentlicht in: | Journal of instrumentation 2019-11, Vol.14 (11), p.C11008-C11008 |
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container_title | Journal of instrumentation |
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creator | Crews, C. Soman, M.R. Lofthouse-Smith, D-D. Allanwood, E.A.H. Stefanov, K.D. Leese, M. Turner, P. Holland, A.D. |
description | The CIS115 is a Teledyne-e2v CMOS image sensor with 1504×2000 pixels of 7 μm pitch. It has a high optical quantum efficiency owing to a multi-layer anti-reflective coating and its backside illuminated construction, and low dark current due to its pinned photodiode 4T pixel architecture. The sensor operates in rolling shutter mode with a frame rate of up to 7.5 fps (if using the whole array), and has a low readout noise of ∼5 electrons rms. The CIS115 has been selected for use within the JANUS instrument, which is a high resolution camera due to launch on board ESA's JUpiter ICy moons Explorer (JUICE) spacecraft in 2022. After an interplanetary transit time of over 7 years, JUICE will spend 3.5 years touring the Jovian system, studying three of the Galilean moons in particular: Ganymede, Callisto and Europa. During this latter part of the mission, the spacecraft and hence the CIS115 sensor will be subjected to the significant levels of trapped radiation surrounding Jupiter. Gamma and proton irradiation campaigns have therefore been undertaken in order to evaluate both ionising and non-ionising dose effects on the CIS115's dark current performance. Characterisations were carried out at expected mission operating temperatures (−35±10ˆC) both prior to and post-irradiation. Models of the resulting degradation in dark current behaviour will be combined with expected doses during the JUICE mission in order to predict the performance of the CIS115 at the mission end-of-life. |
doi_str_mv | 10.1088/1748-0221/14/11/C11008 |
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It has a high optical quantum efficiency owing to a multi-layer anti-reflective coating and its backside illuminated construction, and low dark current due to its pinned photodiode 4T pixel architecture. The sensor operates in rolling shutter mode with a frame rate of up to 7.5 fps (if using the whole array), and has a low readout noise of ∼5 electrons rms. The CIS115 has been selected for use within the JANUS instrument, which is a high resolution camera due to launch on board ESA's JUpiter ICy moons Explorer (JUICE) spacecraft in 2022. After an interplanetary transit time of over 7 years, JUICE will spend 3.5 years touring the Jovian system, studying three of the Galilean moons in particular: Ganymede, Callisto and Europa. During this latter part of the mission, the spacecraft and hence the CIS115 sensor will be subjected to the significant levels of trapped radiation surrounding Jupiter. Gamma and proton irradiation campaigns have therefore been undertaken in order to evaluate both ionising and non-ionising dose effects on the CIS115's dark current performance. Characterisations were carried out at expected mission operating temperatures (−35±10ˆC) both prior to and post-irradiation. Models of the resulting degradation in dark current behaviour will be combined with expected doses during the JUICE mission in order to predict the performance of the CIS115 at the mission end-of-life.</description><identifier>ISSN: 1748-0221</identifier><identifier>EISSN: 1748-0221</identifier><identifier>DOI: 10.1088/1748-0221/14/11/C11008</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Antireflection coatings ; Callisto ; CMOS ; Dark current ; Europa ; Galilean satellites ; Ganymede ; Icy satellites ; Jupiter ; Jupiter satellites ; Multilayers ; Operating temperature ; Photodiodes ; Pixels ; Proton irradiation ; Quantum efficiency ; Radiation damage ; Radiation effects ; Sensors ; Spacecraft ; Transit time</subject><ispartof>Journal of instrumentation, 2019-11, Vol.14 (11), p.C11008-C11008</ispartof><rights>Copyright IOP Publishing Nov 2019</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c331t-fea6127f615cc549b8446231e90da96e1816fc9c452a5ac5be9a1d5bac71f74c3</citedby><cites>FETCH-LOGICAL-c331t-fea6127f615cc549b8446231e90da96e1816fc9c452a5ac5be9a1d5bac71f74c3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,777,781,27905,27906</link.rule.ids></links><search><creatorcontrib>Crews, C.</creatorcontrib><creatorcontrib>Soman, M.R.</creatorcontrib><creatorcontrib>Lofthouse-Smith, D-D.</creatorcontrib><creatorcontrib>Allanwood, E.A.H.</creatorcontrib><creatorcontrib>Stefanov, K.D.</creatorcontrib><creatorcontrib>Leese, M.</creatorcontrib><creatorcontrib>Turner, P.</creatorcontrib><creatorcontrib>Holland, A.D.</creatorcontrib><title>Predicting the effect of radiation damage on dark current in a space-qualified high performance CMOS image sensor</title><title>Journal of instrumentation</title><description>The CIS115 is a Teledyne-e2v CMOS image sensor with 1504×2000 pixels of 7 μm pitch. It has a high optical quantum efficiency owing to a multi-layer anti-reflective coating and its backside illuminated construction, and low dark current due to its pinned photodiode 4T pixel architecture. The sensor operates in rolling shutter mode with a frame rate of up to 7.5 fps (if using the whole array), and has a low readout noise of ∼5 electrons rms. The CIS115 has been selected for use within the JANUS instrument, which is a high resolution camera due to launch on board ESA's JUpiter ICy moons Explorer (JUICE) spacecraft in 2022. After an interplanetary transit time of over 7 years, JUICE will spend 3.5 years touring the Jovian system, studying three of the Galilean moons in particular: Ganymede, Callisto and Europa. During this latter part of the mission, the spacecraft and hence the CIS115 sensor will be subjected to the significant levels of trapped radiation surrounding Jupiter. Gamma and proton irradiation campaigns have therefore been undertaken in order to evaluate both ionising and non-ionising dose effects on the CIS115's dark current performance. Characterisations were carried out at expected mission operating temperatures (−35±10ˆC) both prior to and post-irradiation. Models of the resulting degradation in dark current behaviour will be combined with expected doses during the JUICE mission in order to predict the performance of the CIS115 at the mission end-of-life.</description><subject>Antireflection coatings</subject><subject>Callisto</subject><subject>CMOS</subject><subject>Dark current</subject><subject>Europa</subject><subject>Galilean satellites</subject><subject>Ganymede</subject><subject>Icy satellites</subject><subject>Jupiter</subject><subject>Jupiter satellites</subject><subject>Multilayers</subject><subject>Operating temperature</subject><subject>Photodiodes</subject><subject>Pixels</subject><subject>Proton irradiation</subject><subject>Quantum efficiency</subject><subject>Radiation damage</subject><subject>Radiation effects</subject><subject>Sensors</subject><subject>Spacecraft</subject><subject>Transit time</subject><issn>1748-0221</issn><issn>1748-0221</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNpNkEtPwzAQhC0EEqXwF5AlziHexM7jiCJeEqhIwNnaOuvWpU1S2znw7-kDIU470o5mRh9j1yBuQVRVCqWsEpFlkIJMAdIGQIjqhE3-Hqf_9Dm7CGElhKqVFBO2ffPUOhNdt-BxSZysJRN5b7nH1mF0fcdb3OCC-EH5L25G76mL3HUceRjQULIdce2so5Yv3WLJB_K29xvsDPHmdfbO3SEgUBd6f8nOLK4DXf3eKft8uP9onpKX2eNzc_eSmDyHmFjCArLSFqCMUbKeV1IWWQ5UixbrgqCCwpraSJWhQqPmVCO0ao6mBFtKk0_ZzTF38P12pBD1qh99t6vUWa7KQgpV5jtXcXQZ34fgyerB79b6bw1C7_HqPTm9J6dBagB9xJv_AFQQbjU</recordid><startdate>20191101</startdate><enddate>20191101</enddate><creator>Crews, C.</creator><creator>Soman, M.R.</creator><creator>Lofthouse-Smith, D-D.</creator><creator>Allanwood, E.A.H.</creator><creator>Stefanov, K.D.</creator><creator>Leese, M.</creator><creator>Turner, P.</creator><creator>Holland, A.D.</creator><general>IOP Publishing</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7U5</scope><scope>8FD</scope><scope>L7M</scope></search><sort><creationdate>20191101</creationdate><title>Predicting the effect of radiation damage on dark current in a space-qualified high performance CMOS image sensor</title><author>Crews, C. ; Soman, M.R. ; Lofthouse-Smith, D-D. ; Allanwood, E.A.H. ; Stefanov, K.D. ; Leese, M. ; Turner, P. ; Holland, A.D.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c331t-fea6127f615cc549b8446231e90da96e1816fc9c452a5ac5be9a1d5bac71f74c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Antireflection coatings</topic><topic>Callisto</topic><topic>CMOS</topic><topic>Dark current</topic><topic>Europa</topic><topic>Galilean satellites</topic><topic>Ganymede</topic><topic>Icy satellites</topic><topic>Jupiter</topic><topic>Jupiter satellites</topic><topic>Multilayers</topic><topic>Operating temperature</topic><topic>Photodiodes</topic><topic>Pixels</topic><topic>Proton irradiation</topic><topic>Quantum efficiency</topic><topic>Radiation damage</topic><topic>Radiation effects</topic><topic>Sensors</topic><topic>Spacecraft</topic><topic>Transit time</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Crews, C.</creatorcontrib><creatorcontrib>Soman, M.R.</creatorcontrib><creatorcontrib>Lofthouse-Smith, D-D.</creatorcontrib><creatorcontrib>Allanwood, E.A.H.</creatorcontrib><creatorcontrib>Stefanov, K.D.</creatorcontrib><creatorcontrib>Leese, M.</creatorcontrib><creatorcontrib>Turner, P.</creatorcontrib><creatorcontrib>Holland, A.D.</creatorcontrib><collection>CrossRef</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Technology Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of instrumentation</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Crews, C.</au><au>Soman, M.R.</au><au>Lofthouse-Smith, D-D.</au><au>Allanwood, E.A.H.</au><au>Stefanov, K.D.</au><au>Leese, M.</au><au>Turner, P.</au><au>Holland, A.D.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Predicting the effect of radiation damage on dark current in a space-qualified high performance CMOS image sensor</atitle><jtitle>Journal of instrumentation</jtitle><date>2019-11-01</date><risdate>2019</risdate><volume>14</volume><issue>11</issue><spage>C11008</spage><epage>C11008</epage><pages>C11008-C11008</pages><issn>1748-0221</issn><eissn>1748-0221</eissn><abstract>The CIS115 is a Teledyne-e2v CMOS image sensor with 1504×2000 pixels of 7 μm pitch. It has a high optical quantum efficiency owing to a multi-layer anti-reflective coating and its backside illuminated construction, and low dark current due to its pinned photodiode 4T pixel architecture. The sensor operates in rolling shutter mode with a frame rate of up to 7.5 fps (if using the whole array), and has a low readout noise of ∼5 electrons rms. The CIS115 has been selected for use within the JANUS instrument, which is a high resolution camera due to launch on board ESA's JUpiter ICy moons Explorer (JUICE) spacecraft in 2022. After an interplanetary transit time of over 7 years, JUICE will spend 3.5 years touring the Jovian system, studying three of the Galilean moons in particular: Ganymede, Callisto and Europa. During this latter part of the mission, the spacecraft and hence the CIS115 sensor will be subjected to the significant levels of trapped radiation surrounding Jupiter. Gamma and proton irradiation campaigns have therefore been undertaken in order to evaluate both ionising and non-ionising dose effects on the CIS115's dark current performance. Characterisations were carried out at expected mission operating temperatures (−35±10ˆC) both prior to and post-irradiation. Models of the resulting degradation in dark current behaviour will be combined with expected doses during the JUICE mission in order to predict the performance of the CIS115 at the mission end-of-life.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1748-0221/14/11/C11008</doi><oa>free_for_read</oa></addata></record> |
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subjects | Antireflection coatings Callisto CMOS Dark current Europa Galilean satellites Ganymede Icy satellites Jupiter Jupiter satellites Multilayers Operating temperature Photodiodes Pixels Proton irradiation Quantum efficiency Radiation damage Radiation effects Sensors Spacecraft Transit time |
title | Predicting the effect of radiation damage on dark current in a space-qualified high performance CMOS image sensor |
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