Dust-tolerant mechanism design for lunar & NEO surface systems
NASA has grand goals including exploring extraterrestrial bodies such as near-earth objects (NEOs) in order to better understand our origins as well as protect Earth from space-based threats. Robotic precursor missions and eventually manned exploration will require advanced dust-tolerant mechanisms...
Gespeichert in:
Hauptverfasser: | , , , , |
---|---|
Format: | Tagungsbericht |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 8 |
---|---|
container_issue | |
container_start_page | 1 |
container_title | |
container_volume | |
creator | Herman, J Sadick, S Maksymuk, M Chu, P Carlson, L |
description | NASA has grand goals including exploring extraterrestrial bodies such as near-earth objects (NEOs) in order to better understand our origins as well as protect Earth from space-based threats. Robotic precursor missions and eventually manned exploration will require advanced dust-tolerant mechanisms if long-life and low-risk missions are to be attained. Honeybee Robotics Spacecraft Mechanisms Corporation (Honeybee) has spent the past five years developing scalable, dust-tolerant, utility connectors and related mechanisms with a focus on lunar surface system applications. Solutions in which both load capacity, misalignment tolerances and other aspects can be scaled without an exponential departure from requirements such as mass, volume, and dust-tolerance, enables a modular and scalable system utilizing a standardized interface. At the center of the technology is Honeybee's permeable membrane electrical connector (patent pending). A prototype was successfully tested to 100's of cycles with JSC-1AF lunar simulant at 1 torr and -160°C. Testing has shown that 1000's of cycles is attainable. |
doi_str_mv | 10.1109/AERO.2011.5747264 |
format | Conference Proceeding |
fullrecord | <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_5747264</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>5747264</ieee_id><sourcerecordid>5747264</sourcerecordid><originalsourceid>FETCH-LOGICAL-i175t-d9c45ca5afef6ed2962bb734e3ffdc91c8faa68f2ac13cfef149778f5e3f66a33</originalsourceid><addsrcrecordid>eNo9UMtKxDAUjS9wHOcDxE1W7lLzTrMRhrE-YLAgCu6GTHqjlbYjSbuYvzfg4NmcxXlw70HoitGCMWpvl9VrXXDKWKGMNFzLI3TBJJfSCGnNMZpxazXhQpUn_4Ki9BTNcloRwcXHOVqk9E0zNDcl4zN0dz-lkYy7DqIbRtyD_3JDm3rcQGo_Bxx2EXfT4CK-wS9VjdMUg_OA0z6N0KdLdBZcl2Bx4Dl6f6jeVk9kXT8-r5Zr0jKjRtJYL5V3ygUIGhpuNd9u89kgQmi8Zb4MzukycOeZ8NnE8kemDCobtHZCzNH1X28LAJuf2PYu7jeHHcQv1fFN6A</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Dust-tolerant mechanism design for lunar & NEO surface systems</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Herman, J ; Sadick, S ; Maksymuk, M ; Chu, P ; Carlson, L</creator><creatorcontrib>Herman, J ; Sadick, S ; Maksymuk, M ; Chu, P ; Carlson, L</creatorcontrib><description>NASA has grand goals including exploring extraterrestrial bodies such as near-earth objects (NEOs) in order to better understand our origins as well as protect Earth from space-based threats. Robotic precursor missions and eventually manned exploration will require advanced dust-tolerant mechanisms if long-life and low-risk missions are to be attained. Honeybee Robotics Spacecraft Mechanisms Corporation (Honeybee) has spent the past five years developing scalable, dust-tolerant, utility connectors and related mechanisms with a focus on lunar surface system applications. Solutions in which both load capacity, misalignment tolerances and other aspects can be scaled without an exponential departure from requirements such as mass, volume, and dust-tolerance, enables a modular and scalable system utilizing a standardized interface. At the center of the technology is Honeybee's permeable membrane electrical connector (patent pending). A prototype was successfully tested to 100's of cycles with JSC-1AF lunar simulant at 1 torr and -160°C. Testing has shown that 1000's of cycles is attainable.</description><identifier>ISSN: 1095-323X</identifier><identifier>ISBN: 1424473500</identifier><identifier>ISBN: 9781424473502</identifier><identifier>EISSN: 2996-2358</identifier><identifier>EISBN: 1424473497</identifier><identifier>EISBN: 9781424473519</identifier><identifier>EISBN: 9781424473496</identifier><identifier>EISBN: 1424473519</identifier><identifier>DOI: 10.1109/AERO.2011.5747264</identifier><language>eng</language><publisher>IEEE</publisher><subject>Biomembranes ; Connectors ; Force ; Moon ; Surface topography ; Testing</subject><ispartof>2011 Aerospace Conference, 2011, p.1-8</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/5747264$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2052,27902,54895</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/5747264$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Herman, J</creatorcontrib><creatorcontrib>Sadick, S</creatorcontrib><creatorcontrib>Maksymuk, M</creatorcontrib><creatorcontrib>Chu, P</creatorcontrib><creatorcontrib>Carlson, L</creatorcontrib><title>Dust-tolerant mechanism design for lunar & NEO surface systems</title><title>2011 Aerospace Conference</title><addtitle>AERO</addtitle><description>NASA has grand goals including exploring extraterrestrial bodies such as near-earth objects (NEOs) in order to better understand our origins as well as protect Earth from space-based threats. Robotic precursor missions and eventually manned exploration will require advanced dust-tolerant mechanisms if long-life and low-risk missions are to be attained. Honeybee Robotics Spacecraft Mechanisms Corporation (Honeybee) has spent the past five years developing scalable, dust-tolerant, utility connectors and related mechanisms with a focus on lunar surface system applications. Solutions in which both load capacity, misalignment tolerances and other aspects can be scaled without an exponential departure from requirements such as mass, volume, and dust-tolerance, enables a modular and scalable system utilizing a standardized interface. At the center of the technology is Honeybee's permeable membrane electrical connector (patent pending). A prototype was successfully tested to 100's of cycles with JSC-1AF lunar simulant at 1 torr and -160°C. Testing has shown that 1000's of cycles is attainable.</description><subject>Biomembranes</subject><subject>Connectors</subject><subject>Force</subject><subject>Moon</subject><subject>Surface topography</subject><subject>Testing</subject><issn>1095-323X</issn><issn>2996-2358</issn><isbn>1424473500</isbn><isbn>9781424473502</isbn><isbn>1424473497</isbn><isbn>9781424473519</isbn><isbn>9781424473496</isbn><isbn>1424473519</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2011</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNo9UMtKxDAUjS9wHOcDxE1W7lLzTrMRhrE-YLAgCu6GTHqjlbYjSbuYvzfg4NmcxXlw70HoitGCMWpvl9VrXXDKWKGMNFzLI3TBJJfSCGnNMZpxazXhQpUn_4Ki9BTNcloRwcXHOVqk9E0zNDcl4zN0dz-lkYy7DqIbRtyD_3JDm3rcQGo_Bxx2EXfT4CK-wS9VjdMUg_OA0z6N0KdLdBZcl2Bx4Dl6f6jeVk9kXT8-r5Zr0jKjRtJYL5V3ygUIGhpuNd9u89kgQmi8Zb4MzukycOeZ8NnE8kemDCobtHZCzNH1X28LAJuf2PYu7jeHHcQv1fFN6A</recordid><startdate>201103</startdate><enddate>201103</enddate><creator>Herman, J</creator><creator>Sadick, S</creator><creator>Maksymuk, M</creator><creator>Chu, P</creator><creator>Carlson, L</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>201103</creationdate><title>Dust-tolerant mechanism design for lunar & NEO surface systems</title><author>Herman, J ; Sadick, S ; Maksymuk, M ; Chu, P ; Carlson, L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i175t-d9c45ca5afef6ed2962bb734e3ffdc91c8faa68f2ac13cfef149778f5e3f66a33</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Biomembranes</topic><topic>Connectors</topic><topic>Force</topic><topic>Moon</topic><topic>Surface topography</topic><topic>Testing</topic><toplevel>online_resources</toplevel><creatorcontrib>Herman, J</creatorcontrib><creatorcontrib>Sadick, S</creatorcontrib><creatorcontrib>Maksymuk, M</creatorcontrib><creatorcontrib>Chu, P</creatorcontrib><creatorcontrib>Carlson, L</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Herman, J</au><au>Sadick, S</au><au>Maksymuk, M</au><au>Chu, P</au><au>Carlson, L</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Dust-tolerant mechanism design for lunar & NEO surface systems</atitle><btitle>2011 Aerospace Conference</btitle><stitle>AERO</stitle><date>2011-03</date><risdate>2011</risdate><spage>1</spage><epage>8</epage><pages>1-8</pages><issn>1095-323X</issn><eissn>2996-2358</eissn><isbn>1424473500</isbn><isbn>9781424473502</isbn><eisbn>1424473497</eisbn><eisbn>9781424473519</eisbn><eisbn>9781424473496</eisbn><eisbn>1424473519</eisbn><abstract>NASA has grand goals including exploring extraterrestrial bodies such as near-earth objects (NEOs) in order to better understand our origins as well as protect Earth from space-based threats. Robotic precursor missions and eventually manned exploration will require advanced dust-tolerant mechanisms if long-life and low-risk missions are to be attained. Honeybee Robotics Spacecraft Mechanisms Corporation (Honeybee) has spent the past five years developing scalable, dust-tolerant, utility connectors and related mechanisms with a focus on lunar surface system applications. Solutions in which both load capacity, misalignment tolerances and other aspects can be scaled without an exponential departure from requirements such as mass, volume, and dust-tolerance, enables a modular and scalable system utilizing a standardized interface. At the center of the technology is Honeybee's permeable membrane electrical connector (patent pending). A prototype was successfully tested to 100's of cycles with JSC-1AF lunar simulant at 1 torr and -160°C. Testing has shown that 1000's of cycles is attainable.</abstract><pub>IEEE</pub><doi>10.1109/AERO.2011.5747264</doi><tpages>8</tpages></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | ISSN: 1095-323X |
ispartof | 2011 Aerospace Conference, 2011, p.1-8 |
issn | 1095-323X 2996-2358 |
language | eng |
recordid | cdi_ieee_primary_5747264 |
source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Biomembranes Connectors Force Moon Surface topography Testing |
title | Dust-tolerant mechanism design for lunar & NEO surface systems |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-01T02%3A34%3A54IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-ieee_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Dust-tolerant%20mechanism%20design%20for%20lunar%20&%20NEO%20surface%20systems&rft.btitle=2011%20Aerospace%20Conference&rft.au=Herman,%20J&rft.date=2011-03&rft.spage=1&rft.epage=8&rft.pages=1-8&rft.issn=1095-323X&rft.eissn=2996-2358&rft.isbn=1424473500&rft.isbn_list=9781424473502&rft_id=info:doi/10.1109/AERO.2011.5747264&rft_dat=%3Cieee_6IE%3E5747264%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&rft.eisbn=1424473497&rft.eisbn_list=9781424473519&rft.eisbn_list=9781424473496&rft.eisbn_list=1424473519&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=5747264&rfr_iscdi=true |