Performance Characterization of the TRW 95 K High Efficiency Cryocooler

This paper presents results from characterization studies performed on the Northrop Grumman Space Technology, formerly TRW, 95 K High Efficiency Cryocooler at the Air Force Research Laboratory (AFRL) Cryogenic Technology Research Facility. This pulse tube cryocooler unit is capable of lifting 10 W h...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Yarbrough, S A, Abhyankar, N, Tomlinson, B J, Davis, T M
Format: Tagungsbericht
Sprache:eng
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 1284
container_issue
container_start_page 1277
container_title
container_volume 710
creator Yarbrough, S A
Abhyankar, N
Tomlinson, B J
Davis, T M
description This paper presents results from characterization studies performed on the Northrop Grumman Space Technology, formerly TRW, 95 K High Efficiency Cryocooler at the Air Force Research Laboratory (AFRL) Cryogenic Technology Research Facility. This pulse tube cryocooler unit is capable of lifting 10 W heat loads at 95 K, and has demonstrated the highest efficiency performance at this temperature range for space cryocoolers characterized at AFRL. Physical characteristics of the test setup for the cooler are described in the paper. Results are presented for the cryocooler over a wide range of operating parameters and environmental conditions. Effects of varying heat rejection temperature, compressor drive input, and heat loads on the input power and cold end temperatures are examined as well as the cold end temperature stability. In addition, the effect of orientation on the cryocooler's performance is presented. The cooler has entered life-test mode with accumulation of over 5000 of run-time hours.
doi_str_mv 10.1063/1.1774815
format Conference Proceeding
fullrecord <record><control><sourceid>proquest</sourceid><recordid>TN_cdi_proquest_miscellaneous_29512283</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>29512283</sourcerecordid><originalsourceid>FETCH-LOGICAL-p186t-d3bc355d83dcec8887b4d20c1f53a68e4e1a70ce73ba98b08f3629af55832ddf3</originalsourceid><addsrcrecordid>eNotzLFOwzAQAFBLgEQpHfgDT2wpts-OzyOKSouoBEJFsFWOc6ZBaVycdChfzwDT2x5jN1LMpSjhTs6ltRqlOWMzZ1FYMFoAanHOJkI4XSgNH5fsahi-hFDOWpyw5QvlmPLe94F4tfPZh5Fy--PHNvU8RT7uiG9e37kz_Imv2s8dX8TYhpb6cOJVPqWQUkf5ml1E3w00-3fK3h4Wm2pVrJ-Xj9X9ujhILMeigTqAMQ1CEyggoq11o0SQ0YAvkTRJb0UgC7V3WAuMUCrnozEIqmkiTNnt33vI6ftIw7jdt0OgrvM9peOwVc5IpRDgFzk1Tmk</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype><pqid>29512283</pqid></control><display><type>conference_proceeding</type><title>Performance Characterization of the TRW 95 K High Efficiency Cryocooler</title><source>American Institute of Physics (AIP) Journals</source><creator>Yarbrough, S A ; Abhyankar, N ; Tomlinson, B J ; Davis, T M</creator><creatorcontrib>Yarbrough, S A ; Abhyankar, N ; Tomlinson, B J ; Davis, T M</creatorcontrib><description>This paper presents results from characterization studies performed on the Northrop Grumman Space Technology, formerly TRW, 95 K High Efficiency Cryocooler at the Air Force Research Laboratory (AFRL) Cryogenic Technology Research Facility. This pulse tube cryocooler unit is capable of lifting 10 W heat loads at 95 K, and has demonstrated the highest efficiency performance at this temperature range for space cryocoolers characterized at AFRL. Physical characteristics of the test setup for the cooler are described in the paper. Results are presented for the cryocooler over a wide range of operating parameters and environmental conditions. Effects of varying heat rejection temperature, compressor drive input, and heat loads on the input power and cold end temperatures are examined as well as the cold end temperature stability. In addition, the effect of orientation on the cryocooler's performance is presented. The cooler has entered life-test mode with accumulation of over 5000 of run-time hours.</description><identifier>ISSN: 0094-243X</identifier><identifier>ISBN: 9780735403840</identifier><identifier>ISBN: 0735403848</identifier><identifier>DOI: 10.1063/1.1774815</identifier><language>eng</language><ispartof>Advances in Cryogenic Engineering; Volume 49B, 2004, Vol.710, p.1277-1284</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></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>Yarbrough, S A</creatorcontrib><creatorcontrib>Abhyankar, N</creatorcontrib><creatorcontrib>Tomlinson, B J</creatorcontrib><creatorcontrib>Davis, T M</creatorcontrib><title>Performance Characterization of the TRW 95 K High Efficiency Cryocooler</title><title>Advances in Cryogenic Engineering; Volume 49B</title><description>This paper presents results from characterization studies performed on the Northrop Grumman Space Technology, formerly TRW, 95 K High Efficiency Cryocooler at the Air Force Research Laboratory (AFRL) Cryogenic Technology Research Facility. This pulse tube cryocooler unit is capable of lifting 10 W heat loads at 95 K, and has demonstrated the highest efficiency performance at this temperature range for space cryocoolers characterized at AFRL. Physical characteristics of the test setup for the cooler are described in the paper. Results are presented for the cryocooler over a wide range of operating parameters and environmental conditions. Effects of varying heat rejection temperature, compressor drive input, and heat loads on the input power and cold end temperatures are examined as well as the cold end temperature stability. In addition, the effect of orientation on the cryocooler's performance is presented. The cooler has entered life-test mode with accumulation of over 5000 of run-time hours.</description><issn>0094-243X</issn><isbn>9780735403840</isbn><isbn>0735403848</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2004</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNotzLFOwzAQAFBLgEQpHfgDT2wpts-OzyOKSouoBEJFsFWOc6ZBaVycdChfzwDT2x5jN1LMpSjhTs6ltRqlOWMzZ1FYMFoAanHOJkI4XSgNH5fsahi-hFDOWpyw5QvlmPLe94F4tfPZh5Fy--PHNvU8RT7uiG9e37kz_Imv2s8dX8TYhpb6cOJVPqWQUkf5ml1E3w00-3fK3h4Wm2pVrJ-Xj9X9ujhILMeigTqAMQ1CEyggoq11o0SQ0YAvkTRJb0UgC7V3WAuMUCrnozEIqmkiTNnt33vI6ftIw7jdt0OgrvM9peOwVc5IpRDgFzk1Tmk</recordid><startdate>20040623</startdate><enddate>20040623</enddate><creator>Yarbrough, S A</creator><creator>Abhyankar, N</creator><creator>Tomlinson, B J</creator><creator>Davis, T M</creator><scope>7U5</scope><scope>8FD</scope><scope>L7M</scope></search><sort><creationdate>20040623</creationdate><title>Performance Characterization of the TRW 95 K High Efficiency Cryocooler</title><author>Yarbrough, S A ; Abhyankar, N ; Tomlinson, B J ; Davis, T M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p186t-d3bc355d83dcec8887b4d20c1f53a68e4e1a70ce73ba98b08f3629af55832ddf3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2004</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yarbrough, S A</creatorcontrib><creatorcontrib>Abhyankar, N</creatorcontrib><creatorcontrib>Tomlinson, B J</creatorcontrib><creatorcontrib>Davis, T M</creatorcontrib><collection>Solid State and Superconductivity Abstracts</collection><collection>Technology Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yarbrough, S A</au><au>Abhyankar, N</au><au>Tomlinson, B J</au><au>Davis, T M</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Performance Characterization of the TRW 95 K High Efficiency Cryocooler</atitle><btitle>Advances in Cryogenic Engineering; Volume 49B</btitle><date>2004-06-23</date><risdate>2004</risdate><volume>710</volume><spage>1277</spage><epage>1284</epage><pages>1277-1284</pages><issn>0094-243X</issn><isbn>9780735403840</isbn><isbn>0735403848</isbn><abstract>This paper presents results from characterization studies performed on the Northrop Grumman Space Technology, formerly TRW, 95 K High Efficiency Cryocooler at the Air Force Research Laboratory (AFRL) Cryogenic Technology Research Facility. This pulse tube cryocooler unit is capable of lifting 10 W heat loads at 95 K, and has demonstrated the highest efficiency performance at this temperature range for space cryocoolers characterized at AFRL. Physical characteristics of the test setup for the cooler are described in the paper. Results are presented for the cryocooler over a wide range of operating parameters and environmental conditions. Effects of varying heat rejection temperature, compressor drive input, and heat loads on the input power and cold end temperatures are examined as well as the cold end temperature stability. In addition, the effect of orientation on the cryocooler's performance is presented. The cooler has entered life-test mode with accumulation of over 5000 of run-time hours.</abstract><doi>10.1063/1.1774815</doi><tpages>8</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0094-243X
ispartof Advances in Cryogenic Engineering; Volume 49B, 2004, Vol.710, p.1277-1284
issn 0094-243X
language eng
recordid cdi_proquest_miscellaneous_29512283
source American Institute of Physics (AIP) Journals
title Performance Characterization of the TRW 95 K High Efficiency Cryocooler
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T17%3A57%3A40IST&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:book&rft.genre=proceeding&rft.atitle=Performance%20Characterization%20of%20the%20TRW%2095%20K%20High%20Efficiency%20Cryocooler&rft.btitle=Advances%20in%20Cryogenic%20Engineering;%20Volume%2049B&rft.au=Yarbrough,%20S%20A&rft.date=2004-06-23&rft.volume=710&rft.spage=1277&rft.epage=1284&rft.pages=1277-1284&rft.issn=0094-243X&rft.isbn=9780735403840&rft.isbn_list=0735403848&rft_id=info:doi/10.1063/1.1774815&rft_dat=%3Cproquest%3E29512283%3C/proquest%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=29512283&rft_id=info:pmid/&rfr_iscdi=true