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The Influence of Varying Spacecraft Potentials and Debye Lengths on In Situ Low‐Energy Ion Measurements
Low‐energy ions are difficult to measure, mainly due to spacecraft charging. The ions are attracted to or repelled from the charged surface prior to detection, which changes both the energy and travel direction of the ions. This results in distortions of the data, and the changed travel directions d...
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Published in: | Journal of geophysical research. Space physics 2020-04, Vol.125 (4), p.n/a |
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creator | Bergman, Sofia Stenberg Wieser, Gabriella Wieser, Martin Johansson, Fredrik Leffe Eriksson, Anders |
description | Low‐energy ions are difficult to measure, mainly due to spacecraft charging. The ions are attracted to or repelled from the charged surface prior to detection, which changes both the energy and travel direction of the ions. This results in distortions of the data, and the changed travel directions distort the effective field of view (FOV) of the instrument performing the measurements. The ion composition analyzer (RPC‐ICA) was measuring positive ions down to an energy of a few eV around comet 67P/Churyumov‐Gerasimenko. Low‐energy ions play important parts in processes in the cometary environment, but the FOV of RPC‐ICA has been shown to get severely distorted at low ion energies. Several factors are believed to affect the distortion level. In this study we use the Spacecraft Plasma Interaction Software (SPIS) to investigate the influence of varying spacecraft potentials and Debye lengths on the FOV distortion of RPC‐ICA. We show that the distortion level is dependent on the Debye length of the surrounding plasma, but the sensitivity varies substantially between different viewing directions of the instrument. We also show that a small nonlinearity exists in the relation between FOV distortion, ion energy, and spacecraft potential, mainly caused by the photoemission and bulk flow of the cometary plasma.
Key Points
We model the low‐energy field of view of the ion composition analyzer on Rosetta for varying spacecraft potentials and Debye lengths
The field of view distortion is sensitive to changes in the Debye length, but the sensitivity varies between different viewing directions
A small nonlinearity is found in the relation between field of view distortion, ion energy, and spacecraft potential |
doi_str_mv | 10.1029/2020JA027870 |
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Key Points
We model the low‐energy field of view of the ion composition analyzer on Rosetta for varying spacecraft potentials and Debye lengths
The field of view distortion is sensitive to changes in the Debye length, but the sensitivity varies between different viewing directions
A small nonlinearity is found in the relation between field of view distortion, ion energy, and spacecraft potential</description><identifier>ISSN: 2169-9380</identifier><identifier>ISSN: 2169-9402</identifier><identifier>EISSN: 2169-9402</identifier><identifier>DOI: 10.1029/2020JA027870</identifier><language>eng</language><publisher>Washington: Blackwell Publishing Ltd</publisher><subject>Change detection ; Charging ; comet ; Comets ; Debye length ; Distortion ; Energy ; Field of view ; Ions ; low-energy ions ; Photoelectric emission ; Plasma interactions ; Positive ions ; Rosetta ; rymd- och plasmafysik ; Space and Plasma Physics ; Spacecraft ; Spacecraft charging ; Spacecraft-environment interaction ; SPIS</subject><ispartof>Journal of geophysical research. Space physics, 2020-04, Vol.125 (4), p.n/a</ispartof><rights>2020. The Authors.</rights><rights>2020. This article is published under http://creativecommons.org/licenses/by/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c4208-7b723135cf06e1426dc7cb58c1c76b19207fa56ff71fa06520542c9b8432c2c3</citedby><cites>FETCH-LOGICAL-c4208-7b723135cf06e1426dc7cb58c1c76b19207fa56ff71fa06520542c9b8432c2c3</cites><orcidid>0000-0003-0673-2264 ; 0000-0002-4260-2937 ; 0000-0002-1760-210X ; 0000-0003-2926-6761</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,314,780,784,885,27924,27925</link.rule.ids><backlink>$$Uhttps://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-168032$$DView record from Swedish Publication Index$$Hfree_for_read</backlink><backlink>$$Uhttps://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-417832$$DView record from Swedish Publication Index$$Hfree_for_read</backlink></links><search><creatorcontrib>Bergman, Sofia</creatorcontrib><creatorcontrib>Stenberg Wieser, Gabriella</creatorcontrib><creatorcontrib>Wieser, Martin</creatorcontrib><creatorcontrib>Johansson, Fredrik Leffe</creatorcontrib><creatorcontrib>Eriksson, Anders</creatorcontrib><title>The Influence of Varying Spacecraft Potentials and Debye Lengths on In Situ Low‐Energy Ion Measurements</title><title>Journal of geophysical research. Space physics</title><description>Low‐energy ions are difficult to measure, mainly due to spacecraft charging. The ions are attracted to or repelled from the charged surface prior to detection, which changes both the energy and travel direction of the ions. This results in distortions of the data, and the changed travel directions distort the effective field of view (FOV) of the instrument performing the measurements. The ion composition analyzer (RPC‐ICA) was measuring positive ions down to an energy of a few eV around comet 67P/Churyumov‐Gerasimenko. Low‐energy ions play important parts in processes in the cometary environment, but the FOV of RPC‐ICA has been shown to get severely distorted at low ion energies. Several factors are believed to affect the distortion level. In this study we use the Spacecraft Plasma Interaction Software (SPIS) to investigate the influence of varying spacecraft potentials and Debye lengths on the FOV distortion of RPC‐ICA. We show that the distortion level is dependent on the Debye length of the surrounding plasma, but the sensitivity varies substantially between different viewing directions of the instrument. We also show that a small nonlinearity exists in the relation between FOV distortion, ion energy, and spacecraft potential, mainly caused by the photoemission and bulk flow of the cometary plasma.
Key Points
We model the low‐energy field of view of the ion composition analyzer on Rosetta for varying spacecraft potentials and Debye lengths
The field of view distortion is sensitive to changes in the Debye length, but the sensitivity varies between different viewing directions
A small nonlinearity is found in the relation between field of view distortion, ion energy, and spacecraft potential</description><subject>Change detection</subject><subject>Charging</subject><subject>comet</subject><subject>Comets</subject><subject>Debye length</subject><subject>Distortion</subject><subject>Energy</subject><subject>Field of view</subject><subject>Ions</subject><subject>low-energy ions</subject><subject>Photoelectric emission</subject><subject>Plasma interactions</subject><subject>Positive ions</subject><subject>Rosetta</subject><subject>rymd- och plasmafysik</subject><subject>Space and Plasma Physics</subject><subject>Spacecraft</subject><subject>Spacecraft charging</subject><subject>Spacecraft-environment interaction</subject><subject>SPIS</subject><issn>2169-9380</issn><issn>2169-9402</issn><issn>2169-9402</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><sourceid>24P</sourceid><recordid>eNqNkclOwzAQhiMEEgi48QCWuBLwksTOsWIpRUUgWvVqOWZcglq72LGq3ngEnpEnwVC2E2IuM5r55tcsWXZA8DHBtD6hmOKrHqZccLyR7VBS1XldYLr5FTOBt7P9EB5xMpFSpNzJ2vEDoIE1swhWA3IGTZRftXaKRgulQXtlOnTrOrBdq2YBKXuPzqBZARqCnXYPATmb-tGo7SIauuXr88u5BT9doUEqXIMK0cM8dYe9bMskBdj_9LvZ-OJ8fHqZD2_6g9PeMNcFxSLnDaeMsFIbXAEpaHWvuW5KoYnmVUNqirlRZWUMJ0bhqqS4LKiuG1Ewqqlmu9nRWjYsYREbufDtPG0knWrlWTvpSeenMkZZEC4YTXj-D3weJakE_uAP1_zCu6cIoZOPLnqbFpKU1UXNWDruzxDauxA8mG9dguX7t-TvbyWcrfFlO4PVn6y86t_1yrIqBHsDesKVkQ</recordid><startdate>202004</startdate><enddate>202004</enddate><creator>Bergman, Sofia</creator><creator>Stenberg Wieser, Gabriella</creator><creator>Wieser, Martin</creator><creator>Johansson, Fredrik Leffe</creator><creator>Eriksson, Anders</creator><general>Blackwell Publishing Ltd</general><scope>24P</scope><scope>WIN</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TG</scope><scope>8FD</scope><scope>H8D</scope><scope>KL.</scope><scope>L7M</scope><scope>ADHXS</scope><scope>ADTPV</scope><scope>AOWAS</scope><scope>D8T</scope><scope>D93</scope><scope>ZZAVC</scope><scope>ACNBI</scope><scope>DF2</scope><orcidid>https://orcid.org/0000-0003-0673-2264</orcidid><orcidid>https://orcid.org/0000-0002-4260-2937</orcidid><orcidid>https://orcid.org/0000-0002-1760-210X</orcidid><orcidid>https://orcid.org/0000-0003-2926-6761</orcidid></search><sort><creationdate>202004</creationdate><title>The Influence of Varying Spacecraft Potentials and Debye Lengths on In Situ Low‐Energy Ion Measurements</title><author>Bergman, Sofia ; Stenberg Wieser, Gabriella ; Wieser, Martin ; Johansson, Fredrik Leffe ; Eriksson, Anders</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c4208-7b723135cf06e1426dc7cb58c1c76b19207fa56ff71fa06520542c9b8432c2c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Change detection</topic><topic>Charging</topic><topic>comet</topic><topic>Comets</topic><topic>Debye length</topic><topic>Distortion</topic><topic>Energy</topic><topic>Field of view</topic><topic>Ions</topic><topic>low-energy ions</topic><topic>Photoelectric emission</topic><topic>Plasma interactions</topic><topic>Positive ions</topic><topic>Rosetta</topic><topic>rymd- och plasmafysik</topic><topic>Space and Plasma Physics</topic><topic>Spacecraft</topic><topic>Spacecraft charging</topic><topic>Spacecraft-environment interaction</topic><topic>SPIS</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bergman, Sofia</creatorcontrib><creatorcontrib>Stenberg Wieser, Gabriella</creatorcontrib><creatorcontrib>Wieser, Martin</creatorcontrib><creatorcontrib>Johansson, Fredrik Leffe</creatorcontrib><creatorcontrib>Eriksson, Anders</creatorcontrib><collection>Open Access: Wiley-Blackwell Open Access Journals</collection><collection>Wiley-Blackwell Backfiles (Open access)</collection><collection>CrossRef</collection><collection>Meteorological & Geoastrophysical Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Meteorological & Geoastrophysical Abstracts - Academic</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>SWEPUB Umeå universitet full text</collection><collection>SwePub</collection><collection>SwePub Articles</collection><collection>SWEPUB Freely available online</collection><collection>SWEPUB Umeå universitet</collection><collection>SwePub Articles full text</collection><collection>SWEPUB Uppsala universitet full text</collection><collection>SWEPUB Uppsala universitet</collection><jtitle>Journal of geophysical research. Space physics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bergman, Sofia</au><au>Stenberg Wieser, Gabriella</au><au>Wieser, Martin</au><au>Johansson, Fredrik Leffe</au><au>Eriksson, Anders</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The Influence of Varying Spacecraft Potentials and Debye Lengths on In Situ Low‐Energy Ion Measurements</atitle><jtitle>Journal of geophysical research. Space physics</jtitle><date>2020-04</date><risdate>2020</risdate><volume>125</volume><issue>4</issue><epage>n/a</epage><issn>2169-9380</issn><issn>2169-9402</issn><eissn>2169-9402</eissn><abstract>Low‐energy ions are difficult to measure, mainly due to spacecraft charging. The ions are attracted to or repelled from the charged surface prior to detection, which changes both the energy and travel direction of the ions. This results in distortions of the data, and the changed travel directions distort the effective field of view (FOV) of the instrument performing the measurements. The ion composition analyzer (RPC‐ICA) was measuring positive ions down to an energy of a few eV around comet 67P/Churyumov‐Gerasimenko. Low‐energy ions play important parts in processes in the cometary environment, but the FOV of RPC‐ICA has been shown to get severely distorted at low ion energies. Several factors are believed to affect the distortion level. In this study we use the Spacecraft Plasma Interaction Software (SPIS) to investigate the influence of varying spacecraft potentials and Debye lengths on the FOV distortion of RPC‐ICA. We show that the distortion level is dependent on the Debye length of the surrounding plasma, but the sensitivity varies substantially between different viewing directions of the instrument. We also show that a small nonlinearity exists in the relation between FOV distortion, ion energy, and spacecraft potential, mainly caused by the photoemission and bulk flow of the cometary plasma.
Key Points
We model the low‐energy field of view of the ion composition analyzer on Rosetta for varying spacecraft potentials and Debye lengths
The field of view distortion is sensitive to changes in the Debye length, but the sensitivity varies between different viewing directions
A small nonlinearity is found in the relation between field of view distortion, ion energy, and spacecraft potential</abstract><cop>Washington</cop><pub>Blackwell Publishing Ltd</pub><doi>10.1029/2020JA027870</doi><tpages>17</tpages><orcidid>https://orcid.org/0000-0003-0673-2264</orcidid><orcidid>https://orcid.org/0000-0002-4260-2937</orcidid><orcidid>https://orcid.org/0000-0002-1760-210X</orcidid><orcidid>https://orcid.org/0000-0003-2926-6761</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Change detection Charging comet Comets Debye length Distortion Energy Field of view Ions low-energy ions Photoelectric emission Plasma interactions Positive ions Rosetta rymd- och plasmafysik Space and Plasma Physics Spacecraft Spacecraft charging Spacecraft-environment interaction SPIS |
title | The Influence of Varying Spacecraft Potentials and Debye Lengths on In Situ Low‐Energy Ion Measurements |
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