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dc.contributor.authorKarampudi, Prathyusha
dc.contributor.authorDutta, Atri
dc.date.accessioned2018-07-11T20:49:12Z
dc.date.available2018-07-11T20:49:12Z
dc.date.issued2017
dc.identifier.citationKarampudi, Prathyusha; Dutta, Atri. 2017. De-orbit time of on-orbit debris for laser-based removal methods. 27th AAS/AIAA Space Flight Mechanics Meeting, vol. 160:pp 3521-3530en_US
dc.identifier.isbn978-0-87703-637-1
dc.identifier.issn1081-6003
dc.identifier.otherWOS:000433401100208
dc.identifier.urihttp://www.univelt.com/book=6261
dc.identifier.urihttp://hdl.handle.net/10057/15369
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractThe amount of space debris in the near-Earth space environment poses a major challenge for current and future space missions. Controlling the growth of on-orbit debris utilizing on-orbit debris removal missions is of great importance for sustained space operations. This paper focusses on the laser-based removal of on-orbit debris utilizing the physical process of ablation. We consider the momentum change of the debris due to laser ablation and investigate the de-orbit times for debris that has cubic and spherical shapes. Our focus is on modeling the de-orbiting process as a low-thrust transfer under the action of continuous perturbation forces. We present numerical results for a variety of starting orbits for the debris.en_US
dc.language.isoen_USen_US
dc.publisherUnivelt, Inc.en_US
dc.relation.ispartofseries27th AAS/AIAA Space Flight Mechanics Meeting;v.160
dc.subjectSpace debrisen_US
dc.subjectCollisionen_US
dc.subjectTethersen_US
dc.titleDe-orbit time of on-orbit debris for laser-based removal methodsen_US
dc.typeConference paperen_US
dc.rights.holder© Copyright 1997-2007 Univelt, Incorporated All Rights Reserveden_US


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