Deorbiting small satellites from the ISS using a tether system
This paper presents results of a study conducted for the project IPERDRONE that aims at the design and development of a small re-entry system, able to perform in-orbit operations near the International Space Station (ISS), to reenter the atmosphere, and to land safely on Earth bringing back scientif...
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| Veröffentlicht in: | CEAS space journal 2021-04, Vol.13 (2), p.217-230 |
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| creator | Brunello, Alice Valmorbida, Andrea Lorenzini, Enrico C. Cantoni, Stefania De Stefano Fumo, Mario Fedele, Alberto Gardi, Roberto Votta, Raffaele |
| description | This paper presents results of a study conducted for the project IPERDRONE that aims at the design and development of a small re-entry system, able to perform in-orbit operations near the International Space Station (ISS), to reenter the atmosphere, and to land safely on Earth bringing back scientific payloads/experiments intact from the ISS. The results presented focus on the dynamics of the tethered space drone using the Swing and Release technique in close proximity of the ISS to exchange momentum between the departing IPERDRONE and the ISS, and the active propulsion system needed for the re-entry trajectory. This study could lead to a new technological solution for deorbiting a space vehicle from the ISS that is low cost, safe and free of contamination. |
| doi_str_mv | 10.1007/s12567-020-00337-1 |
| format | Article |
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The results presented focus on the dynamics of the tethered space drone using the Swing and Release technique in close proximity of the ISS to exchange momentum between the departing IPERDRONE and the ISS, and the active propulsion system needed for the re-entry trajectory. 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This study could lead to a new technological solution for deorbiting a space vehicle from the ISS that is low cost, safe and free of contamination.</description><subject>Aerospace Technology and Astronautics</subject><subject>Atmospheric entry</subject><subject>Deorbiting</subject><subject>Engineering</subject><subject>International Space Station</subject><subject>Multinational space ventures</subject><subject>Original Paper</subject><subject>Payloads</subject><subject>Propulsion systems</subject><subject>Reentry trajectories</subject><subject>Small satellites</subject><subject>Space vehicles</subject><issn>1868-2502</issn><issn>1868-2510</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9kE9PwzAMxSMEEtPYF-AUiXPATtq0uSCh8W_SJA6Dc5Su6ejUriPODvv2BIrgxsmW9d6z_WPsEuEaAYobQpnrQoAEAaBUIfCETbDUpZA5wulvD_KczYi2ACAxA8hwwm7v_RCqNra7DafedR0nF33XtdETb8LQ8_ju-WK14gf60jgefZoETkeKvr9gZ43ryM9-6pS9PT68zp_F8uVpMb9birXSKgqPVQmmlK7OmnRSlUEqpsLaNUaDA8QqL4zJnKm1U87oqjRlaWQtC_CN02rKrsbcfRg-Dp6i3Q6HsEsrbfpLYaHyXCWVHFXrMBAF39h9aHsXjhbBfqGyIyqbUNlvVBaTSY0mSuLdxoe_6H9cnwZnagU</recordid><startdate>20210401</startdate><enddate>20210401</enddate><creator>Brunello, Alice</creator><creator>Valmorbida, Andrea</creator><creator>Lorenzini, Enrico C.</creator><creator>Cantoni, Stefania</creator><creator>De Stefano Fumo, Mario</creator><creator>Fedele, Alberto</creator><creator>Gardi, Roberto</creator><creator>Votta, Raffaele</creator><general>Springer Vienna</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0001-7929-7561</orcidid></search><sort><creationdate>20210401</creationdate><title>Deorbiting small satellites from the ISS using a tether system</title><author>Brunello, Alice ; Valmorbida, Andrea ; Lorenzini, Enrico C. ; Cantoni, Stefania ; De Stefano Fumo, Mario ; Fedele, Alberto ; Gardi, Roberto ; Votta, Raffaele</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c363t-e1b80982ad4f510b40f519b1daf960a011b57994a9d6a3a96b898892d270efa63</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Aerospace Technology and Astronautics</topic><topic>Atmospheric entry</topic><topic>Deorbiting</topic><topic>Engineering</topic><topic>International Space Station</topic><topic>Multinational space ventures</topic><topic>Original Paper</topic><topic>Payloads</topic><topic>Propulsion systems</topic><topic>Reentry trajectories</topic><topic>Small satellites</topic><topic>Space vehicles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Brunello, Alice</creatorcontrib><creatorcontrib>Valmorbida, Andrea</creatorcontrib><creatorcontrib>Lorenzini, Enrico C.</creatorcontrib><creatorcontrib>Cantoni, Stefania</creatorcontrib><creatorcontrib>De Stefano Fumo, Mario</creatorcontrib><creatorcontrib>Fedele, Alberto</creatorcontrib><creatorcontrib>Gardi, Roberto</creatorcontrib><creatorcontrib>Votta, Raffaele</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>CEAS space journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Brunello, Alice</au><au>Valmorbida, Andrea</au><au>Lorenzini, Enrico C.</au><au>Cantoni, Stefania</au><au>De Stefano Fumo, Mario</au><au>Fedele, Alberto</au><au>Gardi, Roberto</au><au>Votta, Raffaele</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Deorbiting small satellites from the ISS using a tether system</atitle><jtitle>CEAS space journal</jtitle><stitle>CEAS Space J</stitle><date>2021-04-01</date><risdate>2021</risdate><volume>13</volume><issue>2</issue><spage>217</spage><epage>230</epage><pages>217-230</pages><issn>1868-2502</issn><eissn>1868-2510</eissn><abstract>This paper presents results of a study conducted for the project IPERDRONE that aims at the design and development of a small re-entry system, able to perform in-orbit operations near the International Space Station (ISS), to reenter the atmosphere, and to land safely on Earth bringing back scientific payloads/experiments intact from the ISS. 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| ispartof | CEAS space journal, 2021-04, Vol.13 (2), p.217-230 |
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| language | eng |
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| source | SpringerLink Journals - AutoHoldings |
| subjects | Aerospace Technology and Astronautics Atmospheric entry Deorbiting Engineering International Space Station Multinational space ventures Original Paper Payloads Propulsion systems Reentry trajectories Small satellites Space vehicles |
| title | Deorbiting small satellites from the ISS using a tether system |
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