Please use this identifier to cite or link to this item: http://hdl.handle.net/1893/26996
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dc.contributor.authorPaton, Mark Den_UK
dc.contributor.authorGreen, Simon Fen_UK
dc.contributor.authorBall, Andrew Jen_UK
dc.contributor.authorZarnecki, John Cen_UK
dc.contributor.authorHagermann, Axelen_UK
dc.date.accessioned2018-04-14T00:59:03Z-
dc.date.available2018-04-14T00:59:03Z-
dc.date.issued2016-08-01en_UK
dc.identifier.urihttp://hdl.handle.net/1893/26996-
dc.description.abstractWe compare measurements made by two impact penetrometers of different sizes and with different tip shapes to further understand penetrometer design for performing penetrometry on an asteroid. To this end we re-visit the interpretation of data from the Huygens' penetrometer, ACC-E, that impacted Titan's surface. In addition we investigate the potential of a spacecraft fitted with a penetrometer to bounce using a test rig, built at The Open University (UK).  Analysis of ACC-E laboratory data, obtained from impacts into ∼4 mm diameter gravel, was found to produce an unusual decrease in resistance with depth (force-depth gradient) which was also seen in the Huygens' ACC-E data from Titan and originally interpreted as a wet or moist sand. The downward trend could also be reproduced in a hybrid Discrete Element Model (DEM) if it was assumed that the near surface particles are more readily mobilised than those deeper in the target.  With regard to penetrometer design penetration resistance was found to be sensitive to the ratio of particle to tip diameter. A clear trend was observed with a conical tip penetrometer, X-PEN, of decreasing force-depth gradients with increasing particle sizes most likely due to a transformation from a bulk displacement of material by the penetrating tip to more local interactions. ACC-E, which has a hemispherical tip, was found to produce a wider range of force-depth gradients than X-PEN, which had a conical tip, possibly due to difficulties dislodging jammed particles. Both penetrometers were able to determine particle diameter and mass after post-processing of the data.  Laboratory simulations of landings with the test rig suggest that a large impact penetrometer under certain circumstances could absorb a significant amount of the elastic energy of the spacecraft possibly aiding landing. Alternatively a small impact penetrometer would allow the spacecraft to bounce freely off the surface to make a measurement at another location. © 2016 COSPAR.en_UK
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.relationPaton MD, Green SF, Ball AJ, Zarnecki JC & Hagermann A (2016) Detection of structure in asteroid analogue materials and Titan's regolith by a landing spacecraft. Advances in Space Research, 58 (3), pp. 415-437. https://doi.org/10.1016/j.asr.2016.04.026en_UK
dc.rightsAccepted refereed manuscript of: Paton MD, Green SF, Ball AJ, Zarnecki JC & Hagermann A (2016) Detection of structure in asteroid analogue materials and Titan's regolith by a landing spacecraft, Advances in Space Research, 58 (3), pp. 415-437. DOI: 10.1016/j.asr.2016.04.026 © 2016, Elsevier. Licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/en_UK
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/en_UK
dc.subjectSpacecraften_UK
dc.subjectImpacten_UK
dc.subjectHuygensen_UK
dc.subjectRegolithen_UK
dc.subjectPenetrometeren_UK
dc.subjectAsteroiden_UK
dc.titleDetection of structure in asteroid analogue materials and Titan's regolith by a landing spacecraften_UK
dc.typeJournal Articleen_UK
dc.identifier.doi10.1016/j.asr.2016.04.026en_UK
dc.citation.jtitleAdvances in Space Researchen_UK
dc.citation.issn0273-1177en_UK
dc.citation.volume58en_UK
dc.citation.issue3en_UK
dc.citation.spage415en_UK
dc.citation.epage437en_UK
dc.citation.publicationstatusPublisheden_UK
dc.citation.peerreviewedRefereeden_UK
dc.type.statusAM - Accepted Manuscripten_UK
dc.citation.date30/04/2016en_UK
dc.contributor.affiliationFinnish Meteorological Instituteen_UK
dc.contributor.affiliationThe Open Universityen_UK
dc.contributor.affiliationThe Open Universityen_UK
dc.contributor.affiliationInternational Space Science Instituteen_UK
dc.contributor.affiliationBiological and Environmental Sciencesen_UK
dc.identifier.isiWOS:000379561000013en_UK
dc.identifier.scopusid2-s2.0-84966874215en_UK
dc.identifier.wtid878281en_UK
dc.contributor.orcid0000-0002-1818-9396en_UK
dc.date.accepted2016-04-26en_UK
dcterms.dateAccepted2016-04-26en_UK
dc.date.filedepositdate2018-04-12en_UK
rioxxterms.apcnot requireden_UK
rioxxterms.typeJournal Article/Reviewen_UK
rioxxterms.versionAMen_UK
local.rioxx.authorPaton, Mark D|en_UK
local.rioxx.authorGreen, Simon F|en_UK
local.rioxx.authorBall, Andrew J|en_UK
local.rioxx.authorZarnecki, John C|en_UK
local.rioxx.authorHagermann, Axel|0000-0002-1818-9396en_UK
local.rioxx.projectInternal Project|University of Stirling|https://isni.org/isni/0000000122484331en_UK
local.rioxx.freetoreaddate2018-04-12en_UK
local.rioxx.licencehttp://creativecommons.org/licenses/by-nc-nd/4.0/|2018-04-12|en_UK
local.rioxx.filename1-s2.0-S0273117716301612-main_Green.pdfen_UK
local.rioxx.filecount1en_UK
local.rioxx.source0273-1177en_UK
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