Loading…
PEACE: A PLASMA ELECTRON AND CURRENT EXPERIMENT
An electron analyser to measure the three-dimensional velocity distribution of electrons in the energy range from 0.59 eV to 26.4 keV on the four spacecraft of the Cluster mission is described. The instrument consists of two sensors with hemispherical electrostatic energy analysers with a position-s...
Saved in:
Published in: | Space science reviews 1997-01, Vol.79 (1-2), p.351-398 |
---|---|
Main Authors: | , , , , , , , , , , , , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | cdi_FETCH-LOGICAL-c254t-b937a152a904099c7f31dacac08983c78a123dfdc5f0ee80a3cffb231de8c71d3 |
---|---|
cites | |
container_end_page | 398 |
container_issue | 1-2 |
container_start_page | 351 |
container_title | Space science reviews |
container_volume | 79 |
creator | Johnstone, AD Alsop, C Burge, S Carter, P J Coates, A J Coker, A J Fazakerley, AN Grande, M Gowen, R A Gurgiolo, C Hancock, B K Narheim, B Preece, A Sheather, PH Winningham, J D Woodliffe, R D |
description | An electron analyser to measure the three-dimensional velocity distribution of electrons in the energy range from 0.59 eV to 26.4 keV on the four spacecraft of the Cluster mission is described. The instrument consists of two sensors with hemispherical electrostatic energy analysers with a position-sensitive microchannel plate detectors placed to view radially on opposite sides of the spacecraft. The intrinsic energy resolutions of the two sensors are 12.7% and 16.5% full width at half maximum. Their angular resolutions are 2.8 and 5.3 respectively in an azimuthal direction and 15 in a polar direction. The two sensors will normally measure in different overlapping energy ranges and will scan the distribution in half a spacecraft rotation or 2 s in the overlapped range. While this is the fastest time resolution for complete distributions, partial distributions can be recorded in as little as 62.5 ms and angular distributions at a fixed energy in 7.8 ms. The dynamic range of the instrument is sufficient to provide accurate measurements of the main known populations from the tail lobe to the plasmasheet and the solar wind. While the basic structure of the instrument is conventional, special attention has been paid in the design to improving the precision of the instrument so that a relative accuracy of the order of 1% could be attained in flight in order to measure the gradients between the four spacecraft accurately; to decreasing the minimum energy covered by this technique from 10 eV down to 1 eV; and to providing good three dimensional distributions. |
doi_str_mv | 10.1023/A:1004938001388 |
format | article |
fullrecord | <record><control><sourceid>proquest</sourceid><recordid>TN_cdi_proquest_miscellaneous_954524089</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>27277076</sourcerecordid><originalsourceid>FETCH-LOGICAL-c254t-b937a152a904099c7f31dacac08983c78a123dfdc5f0ee80a3cffb231de8c71d3</originalsourceid><addsrcrecordid>eNp9z71PwzAQBXALgUQpzKwRA7CEnn1Ozu5mpQYqpR8KrcRWuY4jUZUGmvb_xxJMDJ3uDT89vWPslsMTB4EDM-QAUqMC4KjUGevxjESqcxLnrAeAKs0R1CW76rpNNABEPTaYW1PYYWKSeWneJiaxpS0W1WyamOkoKZZVZaeLxL7PbTWexHjNLhq37cLN3-2z5bNdFK9pOXsZF6ZMvcjkIV1rJMcz4TRI0NpTg7x23nlQWqEn5bjAuql91kAIChz6plmLiILyxGvss4ff3q99-30M3WH1-dH5sN26XWiP3UpnMhMytkV5f1IKEkRAeYSPJyHPKS6WXGKkd__opj3ud_HhFaHMc0lS4g9LA2iO</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>734664744</pqid></control><display><type>article</type><title>PEACE: A PLASMA ELECTRON AND CURRENT EXPERIMENT</title><source>Springer Link</source><creator>Johnstone, AD ; Alsop, C ; Burge, S ; Carter, P J ; Coates, A J ; Coker, A J ; Fazakerley, AN ; Grande, M ; Gowen, R A ; Gurgiolo, C ; Hancock, B K ; Narheim, B ; Preece, A ; Sheather, PH ; Winningham, J D ; Woodliffe, R D</creator><creatorcontrib>Johnstone, AD ; Alsop, C ; Burge, S ; Carter, P J ; Coates, A J ; Coker, A J ; Fazakerley, AN ; Grande, M ; Gowen, R A ; Gurgiolo, C ; Hancock, B K ; Narheim, B ; Preece, A ; Sheather, PH ; Winningham, J D ; Woodliffe, R D</creatorcontrib><description>An electron analyser to measure the three-dimensional velocity distribution of electrons in the energy range from 0.59 eV to 26.4 keV on the four spacecraft of the Cluster mission is described. The instrument consists of two sensors with hemispherical electrostatic energy analysers with a position-sensitive microchannel plate detectors placed to view radially on opposite sides of the spacecraft. The intrinsic energy resolutions of the two sensors are 12.7% and 16.5% full width at half maximum. Their angular resolutions are 2.8 and 5.3 respectively in an azimuthal direction and 15 in a polar direction. The two sensors will normally measure in different overlapping energy ranges and will scan the distribution in half a spacecraft rotation or 2 s in the overlapped range. While this is the fastest time resolution for complete distributions, partial distributions can be recorded in as little as 62.5 ms and angular distributions at a fixed energy in 7.8 ms. The dynamic range of the instrument is sufficient to provide accurate measurements of the main known populations from the tail lobe to the plasmasheet and the solar wind. While the basic structure of the instrument is conventional, special attention has been paid in the design to improving the precision of the instrument so that a relative accuracy of the order of 1% could be attained in flight in order to measure the gradients between the four spacecraft accurately; to decreasing the minimum energy covered by this technique from 10 eV down to 1 eV; and to providing good three dimensional distributions.</description><identifier>ISSN: 0038-6308</identifier><identifier>EISSN: 1572-9672</identifier><identifier>DOI: 10.1023/A:1004938001388</identifier><language>eng</language><publisher>Dordrecht: Springer Nature B.V</publisher><subject>Angular distribution ; Angular resolution ; Cluster Mission ; Dynamic range ; Energy ; Energy distribution ; Microchannel plates ; Sensors ; Spacecraft ; Velocity distribution</subject><ispartof>Space science reviews, 1997-01, Vol.79 (1-2), p.351-398</ispartof><rights>Kluwer Academic Publishers 1997</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c254t-b937a152a904099c7f31dacac08983c78a123dfdc5f0ee80a3cffb231de8c71d3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Johnstone, AD</creatorcontrib><creatorcontrib>Alsop, C</creatorcontrib><creatorcontrib>Burge, S</creatorcontrib><creatorcontrib>Carter, P J</creatorcontrib><creatorcontrib>Coates, A J</creatorcontrib><creatorcontrib>Coker, A J</creatorcontrib><creatorcontrib>Fazakerley, AN</creatorcontrib><creatorcontrib>Grande, M</creatorcontrib><creatorcontrib>Gowen, R A</creatorcontrib><creatorcontrib>Gurgiolo, C</creatorcontrib><creatorcontrib>Hancock, B K</creatorcontrib><creatorcontrib>Narheim, B</creatorcontrib><creatorcontrib>Preece, A</creatorcontrib><creatorcontrib>Sheather, PH</creatorcontrib><creatorcontrib>Winningham, J D</creatorcontrib><creatorcontrib>Woodliffe, R D</creatorcontrib><title>PEACE: A PLASMA ELECTRON AND CURRENT EXPERIMENT</title><title>Space science reviews</title><description>An electron analyser to measure the three-dimensional velocity distribution of electrons in the energy range from 0.59 eV to 26.4 keV on the four spacecraft of the Cluster mission is described. The instrument consists of two sensors with hemispherical electrostatic energy analysers with a position-sensitive microchannel plate detectors placed to view radially on opposite sides of the spacecraft. The intrinsic energy resolutions of the two sensors are 12.7% and 16.5% full width at half maximum. Their angular resolutions are 2.8 and 5.3 respectively in an azimuthal direction and 15 in a polar direction. The two sensors will normally measure in different overlapping energy ranges and will scan the distribution in half a spacecraft rotation or 2 s in the overlapped range. While this is the fastest time resolution for complete distributions, partial distributions can be recorded in as little as 62.5 ms and angular distributions at a fixed energy in 7.8 ms. The dynamic range of the instrument is sufficient to provide accurate measurements of the main known populations from the tail lobe to the plasmasheet and the solar wind. While the basic structure of the instrument is conventional, special attention has been paid in the design to improving the precision of the instrument so that a relative accuracy of the order of 1% could be attained in flight in order to measure the gradients between the four spacecraft accurately; to decreasing the minimum energy covered by this technique from 10 eV down to 1 eV; and to providing good three dimensional distributions.</description><subject>Angular distribution</subject><subject>Angular resolution</subject><subject>Cluster Mission</subject><subject>Dynamic range</subject><subject>Energy</subject><subject>Energy distribution</subject><subject>Microchannel plates</subject><subject>Sensors</subject><subject>Spacecraft</subject><subject>Velocity distribution</subject><issn>0038-6308</issn><issn>1572-9672</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1997</creationdate><recordtype>article</recordtype><recordid>eNp9z71PwzAQBXALgUQpzKwRA7CEnn1Ozu5mpQYqpR8KrcRWuY4jUZUGmvb_xxJMDJ3uDT89vWPslsMTB4EDM-QAUqMC4KjUGevxjESqcxLnrAeAKs0R1CW76rpNNABEPTaYW1PYYWKSeWneJiaxpS0W1WyamOkoKZZVZaeLxL7PbTWexHjNLhq37cLN3-2z5bNdFK9pOXsZF6ZMvcjkIV1rJMcz4TRI0NpTg7x23nlQWqEn5bjAuql91kAIChz6plmLiILyxGvss4ff3q99-30M3WH1-dH5sN26XWiP3UpnMhMytkV5f1IKEkRAeYSPJyHPKS6WXGKkd__opj3ud_HhFaHMc0lS4g9LA2iO</recordid><startdate>19970101</startdate><enddate>19970101</enddate><creator>Johnstone, AD</creator><creator>Alsop, C</creator><creator>Burge, S</creator><creator>Carter, P J</creator><creator>Coates, A J</creator><creator>Coker, A J</creator><creator>Fazakerley, AN</creator><creator>Grande, M</creator><creator>Gowen, R A</creator><creator>Gurgiolo, C</creator><creator>Hancock, B K</creator><creator>Narheim, B</creator><creator>Preece, A</creator><creator>Sheather, PH</creator><creator>Winningham, J D</creator><creator>Woodliffe, R D</creator><general>Springer Nature B.V</general><scope>3V.</scope><scope>7TG</scope><scope>7XB</scope><scope>88I</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>GNUQQ</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>KL.</scope><scope>L7M</scope><scope>M2P</scope><scope>P5Z</scope><scope>P62</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>Q9U</scope></search><sort><creationdate>19970101</creationdate><title>PEACE: A PLASMA ELECTRON AND CURRENT EXPERIMENT</title><author>Johnstone, AD ; Alsop, C ; Burge, S ; Carter, P J ; Coates, A J ; Coker, A J ; Fazakerley, AN ; Grande, M ; Gowen, R A ; Gurgiolo, C ; Hancock, B K ; Narheim, B ; Preece, A ; Sheather, PH ; Winningham, J D ; Woodliffe, R D</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c254t-b937a152a904099c7f31dacac08983c78a123dfdc5f0ee80a3cffb231de8c71d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1997</creationdate><topic>Angular distribution</topic><topic>Angular resolution</topic><topic>Cluster Mission</topic><topic>Dynamic range</topic><topic>Energy</topic><topic>Energy distribution</topic><topic>Microchannel plates</topic><topic>Sensors</topic><topic>Spacecraft</topic><topic>Velocity distribution</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Johnstone, AD</creatorcontrib><creatorcontrib>Alsop, C</creatorcontrib><creatorcontrib>Burge, S</creatorcontrib><creatorcontrib>Carter, P J</creatorcontrib><creatorcontrib>Coates, A J</creatorcontrib><creatorcontrib>Coker, A J</creatorcontrib><creatorcontrib>Fazakerley, AN</creatorcontrib><creatorcontrib>Grande, M</creatorcontrib><creatorcontrib>Gowen, R A</creatorcontrib><creatorcontrib>Gurgiolo, C</creatorcontrib><creatorcontrib>Hancock, B K</creatorcontrib><creatorcontrib>Narheim, B</creatorcontrib><creatorcontrib>Preece, A</creatorcontrib><creatorcontrib>Sheather, PH</creatorcontrib><creatorcontrib>Winningham, J D</creatorcontrib><creatorcontrib>Woodliffe, R D</creatorcontrib><collection>ProQuest Central (Corporate)</collection><collection>Meteorological & Geoastrophysical Abstracts</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Science Database (Alumni Edition)</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>ProQuest Central Student</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>Meteorological & Geoastrophysical Abstracts - Academic</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Science Database</collection><collection>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central Basic</collection><jtitle>Space science reviews</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Johnstone, AD</au><au>Alsop, C</au><au>Burge, S</au><au>Carter, P J</au><au>Coates, A J</au><au>Coker, A J</au><au>Fazakerley, AN</au><au>Grande, M</au><au>Gowen, R A</au><au>Gurgiolo, C</au><au>Hancock, B K</au><au>Narheim, B</au><au>Preece, A</au><au>Sheather, PH</au><au>Winningham, J D</au><au>Woodliffe, R D</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>PEACE: A PLASMA ELECTRON AND CURRENT EXPERIMENT</atitle><jtitle>Space science reviews</jtitle><date>1997-01-01</date><risdate>1997</risdate><volume>79</volume><issue>1-2</issue><spage>351</spage><epage>398</epage><pages>351-398</pages><issn>0038-6308</issn><eissn>1572-9672</eissn><abstract>An electron analyser to measure the three-dimensional velocity distribution of electrons in the energy range from 0.59 eV to 26.4 keV on the four spacecraft of the Cluster mission is described. The instrument consists of two sensors with hemispherical electrostatic energy analysers with a position-sensitive microchannel plate detectors placed to view radially on opposite sides of the spacecraft. The intrinsic energy resolutions of the two sensors are 12.7% and 16.5% full width at half maximum. Their angular resolutions are 2.8 and 5.3 respectively in an azimuthal direction and 15 in a polar direction. The two sensors will normally measure in different overlapping energy ranges and will scan the distribution in half a spacecraft rotation or 2 s in the overlapped range. While this is the fastest time resolution for complete distributions, partial distributions can be recorded in as little as 62.5 ms and angular distributions at a fixed energy in 7.8 ms. The dynamic range of the instrument is sufficient to provide accurate measurements of the main known populations from the tail lobe to the plasmasheet and the solar wind. While the basic structure of the instrument is conventional, special attention has been paid in the design to improving the precision of the instrument so that a relative accuracy of the order of 1% could be attained in flight in order to measure the gradients between the four spacecraft accurately; to decreasing the minimum energy covered by this technique from 10 eV down to 1 eV; and to providing good three dimensional distributions.</abstract><cop>Dordrecht</cop><pub>Springer Nature B.V</pub><doi>10.1023/A:1004938001388</doi><tpages>48</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0038-6308 |
ispartof | Space science reviews, 1997-01, Vol.79 (1-2), p.351-398 |
issn | 0038-6308 1572-9672 |
language | eng |
recordid | cdi_proquest_miscellaneous_954524089 |
source | Springer Link |
subjects | Angular distribution Angular resolution Cluster Mission Dynamic range Energy Energy distribution Microchannel plates Sensors Spacecraft Velocity distribution |
title | PEACE: A PLASMA ELECTRON AND CURRENT EXPERIMENT |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T21%3A27%3A36IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=PEACE:%20A%20PLASMA%20ELECTRON%20AND%20CURRENT%20EXPERIMENT&rft.jtitle=Space%20science%20reviews&rft.au=Johnstone,%20AD&rft.date=1997-01-01&rft.volume=79&rft.issue=1-2&rft.spage=351&rft.epage=398&rft.pages=351-398&rft.issn=0038-6308&rft.eissn=1572-9672&rft_id=info:doi/10.1023/A:1004938001388&rft_dat=%3Cproquest%3E27277076%3C/proquest%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c254t-b937a152a904099c7f31dacac08983c78a123dfdc5f0ee80a3cffb231de8c71d3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=734664744&rft_id=info:pmid/&rfr_iscdi=true |