Ejecta from impacts at 0.2–2.3 m/s in low gravity
Collisions between planetary ring particles and in some protoplanetary disk environments occur at speeds below 10 m/s. The particles involved in these low-velocity collisions have negligible gravity and may be made of or coated with smaller dust grains and aggregates. We undertook microgravity impac...
Gespeichert in:
Veröffentlicht in: | Icarus (New York, N.Y. 1962) N.Y. 1962), 2008-06, Vol.195 (2), p.908-917 |
---|---|
Hauptverfasser: | , , , , , , , , , , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 917 |
---|---|
container_issue | 2 |
container_start_page | 908 |
container_title | Icarus (New York, N.Y. 1962) |
container_volume | 195 |
creator | Colwell, Joshua E. Sture, Stein Cintala, Mark Durda, Dan Hendrix, Amanda Goudie, Tyler Curtis, Darren Ashcom, Daniel J. Kanter, Matthew Keohane, Thomas Lemos, Andreas Lupton, Michael Route, Matthew |
description | Collisions between planetary ring particles and in some protoplanetary disk environments occur at speeds below 10 m/s. The particles involved in these low-velocity collisions have negligible gravity and may be made of or coated with smaller dust grains and aggregates. We undertook microgravity impact experiments to better understand the dissipation of energy and production of ejecta in these collisions. Here we report the results of impact experiments of solid projectiles into beds of granular material at impact velocities from 0.2 to 2.3 m/s performed under near-weightless conditions on the NASA KC-135 Weightless Wonder V. Impactors of various densities and radii of 1 and 2 cm were launched into targets of quartz sand, JSC-1 lunar regolith simulant, and JSC-Mars-1 martian regolith simulant. Most impacts were at normal or near-normal incidence angles, though some impacts were at oblique angles. Oblique impacts led to much higher ejection velocities and ejecta masses than normal impacts. For normal incidence impacts, characteristic ejecta velocities increase with impactor kinetic energy,
KE, as approximately
KE
0.5. Ejecta masses could not be measured accurately due to the nature of the experiment, but qualitatively also increased with impactor kinetic energy. Some experiments were near the threshold velocity of 0.2 m/s identified in previous microgravity impact experiments as the minimum velocity needed to produce ejecta [Colwell, J.E., 2003. Icarus 164, 188–196], and the experimental scatter is large at these low speeds in the airplane experiment. A more precise exploration of the transition from low-ejecta-mass impacts to high-ejecta-mass impacts requires a longer and smoother period of reduced gravity. Coefficient of restitution measurements are not possible due to the varying acceleration of the airplane throughout the experiment. |
doi_str_mv | 10.1016/j.icarus.2007.12.019 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_19479640</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0019103508000298</els_id><sourcerecordid>19479640</sourcerecordid><originalsourceid>FETCH-LOGICAL-a390t-fa11d1e7f11730a6ed986070e2089e6c246065c47d0865e47fb530e698ec8c53</originalsourceid><addsrcrecordid>eNp9kMtOwzAQRS0EEqXwByy8gV3SsZ049gYJVbykSmy6t4wzQY7yKHZa1B3_wB_yJaRKxZLVSKNz72gOIdcMUgZMLurUOxu2MeUARcp4CkyfkBkDDQmXmTglMxhXCQORn5OLGGsAyJUWMyIeanSDpVXoW-rbjXVDpHagkPKfr2-eCtouIvUdbfpP-h7szg_7S3JW2Sbi1XHOyfrxYb18TlavTy_L-1VihYYhqSxjJcOiYqwQYCWWWkkoADkojdLxTILMXVaUoGSOWVG95QJQaoVOuVzMye1Uuwn9xxbjYFofHTaN7bDfRsN0VmiZwQhmE-hCH2PAymyCb23YGwbmIMjUZhJkDoIM42a0McZujv02OttUwXbOx78sB6GyXB3q7yYOx193HoOJzmPnsPRhdGfK3v9_6BdGAXst</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>19479640</pqid></control><display><type>article</type><title>Ejecta from impacts at 0.2–2.3 m/s in low gravity</title><source>ScienceDirect Journals (5 years ago - present)</source><creator>Colwell, Joshua E. ; Sture, Stein ; Cintala, Mark ; Durda, Dan ; Hendrix, Amanda ; Goudie, Tyler ; Curtis, Darren ; Ashcom, Daniel J. ; Kanter, Matthew ; Keohane, Thomas ; Lemos, Andreas ; Lupton, Michael ; Route, Matthew</creator><creatorcontrib>Colwell, Joshua E. ; Sture, Stein ; Cintala, Mark ; Durda, Dan ; Hendrix, Amanda ; Goudie, Tyler ; Curtis, Darren ; Ashcom, Daniel J. ; Kanter, Matthew ; Keohane, Thomas ; Lemos, Andreas ; Lupton, Michael ; Route, Matthew</creatorcontrib><description>Collisions between planetary ring particles and in some protoplanetary disk environments occur at speeds below 10 m/s. The particles involved in these low-velocity collisions have negligible gravity and may be made of or coated with smaller dust grains and aggregates. We undertook microgravity impact experiments to better understand the dissipation of energy and production of ejecta in these collisions. Here we report the results of impact experiments of solid projectiles into beds of granular material at impact velocities from 0.2 to 2.3 m/s performed under near-weightless conditions on the NASA KC-135 Weightless Wonder V. Impactors of various densities and radii of 1 and 2 cm were launched into targets of quartz sand, JSC-1 lunar regolith simulant, and JSC-Mars-1 martian regolith simulant. Most impacts were at normal or near-normal incidence angles, though some impacts were at oblique angles. Oblique impacts led to much higher ejection velocities and ejecta masses than normal impacts. For normal incidence impacts, characteristic ejecta velocities increase with impactor kinetic energy,
KE, as approximately
KE
0.5. Ejecta masses could not be measured accurately due to the nature of the experiment, but qualitatively also increased with impactor kinetic energy. Some experiments were near the threshold velocity of 0.2 m/s identified in previous microgravity impact experiments as the minimum velocity needed to produce ejecta [Colwell, J.E., 2003. Icarus 164, 188–196], and the experimental scatter is large at these low speeds in the airplane experiment. A more precise exploration of the transition from low-ejecta-mass impacts to high-ejecta-mass impacts requires a longer and smoother period of reduced gravity. Coefficient of restitution measurements are not possible due to the varying acceleration of the airplane throughout the experiment.</description><identifier>ISSN: 0019-1035</identifier><identifier>EISSN: 1090-2643</identifier><identifier>DOI: 10.1016/j.icarus.2007.12.019</identifier><identifier>CODEN: ICRSA5</identifier><language>eng</language><publisher>San Diego, CA: Elsevier Inc</publisher><subject>Astronomy ; Collisional physics ; Earth, ocean, space ; Exact sciences and technology ; Impact processes ; Planetesimals ; Solar system</subject><ispartof>Icarus (New York, N.Y. 1962), 2008-06, Vol.195 (2), p.908-917</ispartof><rights>2008 Elsevier Inc.</rights><rights>2008 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a390t-fa11d1e7f11730a6ed986070e2089e6c246065c47d0865e47fb530e698ec8c53</citedby><cites>FETCH-LOGICAL-a390t-fa11d1e7f11730a6ed986070e2089e6c246065c47d0865e47fb530e698ec8c53</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.icarus.2007.12.019$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3548,27923,27924,45994</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=20384580$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Colwell, Joshua E.</creatorcontrib><creatorcontrib>Sture, Stein</creatorcontrib><creatorcontrib>Cintala, Mark</creatorcontrib><creatorcontrib>Durda, Dan</creatorcontrib><creatorcontrib>Hendrix, Amanda</creatorcontrib><creatorcontrib>Goudie, Tyler</creatorcontrib><creatorcontrib>Curtis, Darren</creatorcontrib><creatorcontrib>Ashcom, Daniel J.</creatorcontrib><creatorcontrib>Kanter, Matthew</creatorcontrib><creatorcontrib>Keohane, Thomas</creatorcontrib><creatorcontrib>Lemos, Andreas</creatorcontrib><creatorcontrib>Lupton, Michael</creatorcontrib><creatorcontrib>Route, Matthew</creatorcontrib><title>Ejecta from impacts at 0.2–2.3 m/s in low gravity</title><title>Icarus (New York, N.Y. 1962)</title><description>Collisions between planetary ring particles and in some protoplanetary disk environments occur at speeds below 10 m/s. The particles involved in these low-velocity collisions have negligible gravity and may be made of or coated with smaller dust grains and aggregates. We undertook microgravity impact experiments to better understand the dissipation of energy and production of ejecta in these collisions. Here we report the results of impact experiments of solid projectiles into beds of granular material at impact velocities from 0.2 to 2.3 m/s performed under near-weightless conditions on the NASA KC-135 Weightless Wonder V. Impactors of various densities and radii of 1 and 2 cm were launched into targets of quartz sand, JSC-1 lunar regolith simulant, and JSC-Mars-1 martian regolith simulant. Most impacts were at normal or near-normal incidence angles, though some impacts were at oblique angles. Oblique impacts led to much higher ejection velocities and ejecta masses than normal impacts. For normal incidence impacts, characteristic ejecta velocities increase with impactor kinetic energy,
KE, as approximately
KE
0.5. Ejecta masses could not be measured accurately due to the nature of the experiment, but qualitatively also increased with impactor kinetic energy. Some experiments were near the threshold velocity of 0.2 m/s identified in previous microgravity impact experiments as the minimum velocity needed to produce ejecta [Colwell, J.E., 2003. Icarus 164, 188–196], and the experimental scatter is large at these low speeds in the airplane experiment. A more precise exploration of the transition from low-ejecta-mass impacts to high-ejecta-mass impacts requires a longer and smoother period of reduced gravity. Coefficient of restitution measurements are not possible due to the varying acceleration of the airplane throughout the experiment.</description><subject>Astronomy</subject><subject>Collisional physics</subject><subject>Earth, ocean, space</subject><subject>Exact sciences and technology</subject><subject>Impact processes</subject><subject>Planetesimals</subject><subject>Solar system</subject><issn>0019-1035</issn><issn>1090-2643</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><recordid>eNp9kMtOwzAQRS0EEqXwByy8gV3SsZ049gYJVbykSmy6t4wzQY7yKHZa1B3_wB_yJaRKxZLVSKNz72gOIdcMUgZMLurUOxu2MeUARcp4CkyfkBkDDQmXmTglMxhXCQORn5OLGGsAyJUWMyIeanSDpVXoW-rbjXVDpHagkPKfr2-eCtouIvUdbfpP-h7szg_7S3JW2Sbi1XHOyfrxYb18TlavTy_L-1VihYYhqSxjJcOiYqwQYCWWWkkoADkojdLxTILMXVaUoGSOWVG95QJQaoVOuVzMye1Uuwn9xxbjYFofHTaN7bDfRsN0VmiZwQhmE-hCH2PAymyCb23YGwbmIMjUZhJkDoIM42a0McZujv02OttUwXbOx78sB6GyXB3q7yYOx193HoOJzmPnsPRhdGfK3v9_6BdGAXst</recordid><startdate>20080601</startdate><enddate>20080601</enddate><creator>Colwell, Joshua E.</creator><creator>Sture, Stein</creator><creator>Cintala, Mark</creator><creator>Durda, Dan</creator><creator>Hendrix, Amanda</creator><creator>Goudie, Tyler</creator><creator>Curtis, Darren</creator><creator>Ashcom, Daniel J.</creator><creator>Kanter, Matthew</creator><creator>Keohane, Thomas</creator><creator>Lemos, Andreas</creator><creator>Lupton, Michael</creator><creator>Route, Matthew</creator><general>Elsevier Inc</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TG</scope><scope>KL.</scope></search><sort><creationdate>20080601</creationdate><title>Ejecta from impacts at 0.2–2.3 m/s in low gravity</title><author>Colwell, Joshua E. ; Sture, Stein ; Cintala, Mark ; Durda, Dan ; Hendrix, Amanda ; Goudie, Tyler ; Curtis, Darren ; Ashcom, Daniel J. ; Kanter, Matthew ; Keohane, Thomas ; Lemos, Andreas ; Lupton, Michael ; Route, Matthew</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a390t-fa11d1e7f11730a6ed986070e2089e6c246065c47d0865e47fb530e698ec8c53</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2008</creationdate><topic>Astronomy</topic><topic>Collisional physics</topic><topic>Earth, ocean, space</topic><topic>Exact sciences and technology</topic><topic>Impact processes</topic><topic>Planetesimals</topic><topic>Solar system</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Colwell, Joshua E.</creatorcontrib><creatorcontrib>Sture, Stein</creatorcontrib><creatorcontrib>Cintala, Mark</creatorcontrib><creatorcontrib>Durda, Dan</creatorcontrib><creatorcontrib>Hendrix, Amanda</creatorcontrib><creatorcontrib>Goudie, Tyler</creatorcontrib><creatorcontrib>Curtis, Darren</creatorcontrib><creatorcontrib>Ashcom, Daniel J.</creatorcontrib><creatorcontrib>Kanter, Matthew</creatorcontrib><creatorcontrib>Keohane, Thomas</creatorcontrib><creatorcontrib>Lemos, Andreas</creatorcontrib><creatorcontrib>Lupton, Michael</creatorcontrib><creatorcontrib>Route, Matthew</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Meteorological & Geoastrophysical Abstracts</collection><collection>Meteorological & Geoastrophysical Abstracts - Academic</collection><jtitle>Icarus (New York, N.Y. 1962)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Colwell, Joshua E.</au><au>Sture, Stein</au><au>Cintala, Mark</au><au>Durda, Dan</au><au>Hendrix, Amanda</au><au>Goudie, Tyler</au><au>Curtis, Darren</au><au>Ashcom, Daniel J.</au><au>Kanter, Matthew</au><au>Keohane, Thomas</au><au>Lemos, Andreas</au><au>Lupton, Michael</au><au>Route, Matthew</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Ejecta from impacts at 0.2–2.3 m/s in low gravity</atitle><jtitle>Icarus (New York, N.Y. 1962)</jtitle><date>2008-06-01</date><risdate>2008</risdate><volume>195</volume><issue>2</issue><spage>908</spage><epage>917</epage><pages>908-917</pages><issn>0019-1035</issn><eissn>1090-2643</eissn><coden>ICRSA5</coden><abstract>Collisions between planetary ring particles and in some protoplanetary disk environments occur at speeds below 10 m/s. The particles involved in these low-velocity collisions have negligible gravity and may be made of or coated with smaller dust grains and aggregates. We undertook microgravity impact experiments to better understand the dissipation of energy and production of ejecta in these collisions. Here we report the results of impact experiments of solid projectiles into beds of granular material at impact velocities from 0.2 to 2.3 m/s performed under near-weightless conditions on the NASA KC-135 Weightless Wonder V. Impactors of various densities and radii of 1 and 2 cm were launched into targets of quartz sand, JSC-1 lunar regolith simulant, and JSC-Mars-1 martian regolith simulant. Most impacts were at normal or near-normal incidence angles, though some impacts were at oblique angles. Oblique impacts led to much higher ejection velocities and ejecta masses than normal impacts. For normal incidence impacts, characteristic ejecta velocities increase with impactor kinetic energy,
KE, as approximately
KE
0.5. Ejecta masses could not be measured accurately due to the nature of the experiment, but qualitatively also increased with impactor kinetic energy. Some experiments were near the threshold velocity of 0.2 m/s identified in previous microgravity impact experiments as the minimum velocity needed to produce ejecta [Colwell, J.E., 2003. Icarus 164, 188–196], and the experimental scatter is large at these low speeds in the airplane experiment. A more precise exploration of the transition from low-ejecta-mass impacts to high-ejecta-mass impacts requires a longer and smoother period of reduced gravity. Coefficient of restitution measurements are not possible due to the varying acceleration of the airplane throughout the experiment.</abstract><cop>San Diego, CA</cop><pub>Elsevier Inc</pub><doi>10.1016/j.icarus.2007.12.019</doi><tpages>10</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0019-1035 |
ispartof | Icarus (New York, N.Y. 1962), 2008-06, Vol.195 (2), p.908-917 |
issn | 0019-1035 1090-2643 |
language | eng |
recordid | cdi_proquest_miscellaneous_19479640 |
source | ScienceDirect Journals (5 years ago - present) |
subjects | Astronomy Collisional physics Earth, ocean, space Exact sciences and technology Impact processes Planetesimals Solar system |
title | Ejecta from impacts at 0.2–2.3 m/s in low gravity |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-10T23%3A45%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Ejecta%20from%20impacts%20at%200.2%E2%80%932.3%20m/s%20in%20low%20gravity&rft.jtitle=Icarus%20(New%20York,%20N.Y.%201962)&rft.au=Colwell,%20Joshua%20E.&rft.date=2008-06-01&rft.volume=195&rft.issue=2&rft.spage=908&rft.epage=917&rft.pages=908-917&rft.issn=0019-1035&rft.eissn=1090-2643&rft.coden=ICRSA5&rft_id=info:doi/10.1016/j.icarus.2007.12.019&rft_dat=%3Cproquest_cross%3E19479640%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=19479640&rft_id=info:pmid/&rft_els_id=S0019103508000298&rfr_iscdi=true |