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1. Identity statement Reference Type Journal Article Site mtc-m21c.sid.inpe.br Holder Code isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S Identifier 8JMKD3MGP3W34R/3S8PJLS Repository sid.inpe.br/mtc-m21c/2018/11.19.16.07   (restricted access) Last Update 2018:11.19.16.07.28 (UTC) administrator Metadata Repository sid.inpe.br/mtc-m21c/2018/11.19.16.07.28 Metadata Last Update 2021:02.11.18.10.46 (UTC) administrator DOI 10.1007/s40295-017-0120-x ISSN 0021-9142 Citation Key PradoGomeChan:2018:Bu“EPo Title Building an “Escape Portal” with tethers fixed in asteroids Year 2018 Month Sept. Access Date 2024, May 08 Type of Work journal article Secondary Type PRE PI Local Number of Files 1 Size 1287 KiB 2. Context Author 1 Prado, Antonio Fernando Bertachini de Almeida 2 Gomes, Vivian Martins 3 Chanut, Thierry Gregory Gil Resume Identifier 1 8JMKD3MGP5W/3C9JGJA Group 1 DIDMC-CGETE-INPE-MCTIC-GOV-BR Affiliation 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Universidade Estadual Paulista (UNESP) 3 Universidade Estadual Paulista (UNESP) Author e-Mail Address 1 antonio.prado@inpe.br 2 vivianmartinsgomes@gmail.com 3 chiant69@hotmail.com Journal The Journal of the Astronautical Sciences Volume 65 Number 3 Pages 355-375 Secondary Mark B1_ENGENHARIAS_III B5_ASTRONOMIA_/_FÍSICA History (UTC) 2018-12-21 14:26:40 :: simone -> administrator :: 2018 2021-02-11 18:10:46 :: administrator -> simone :: 2018 3. Content and structure Is the master or a copy? is the master Content Stage completed Transferable 1 Content Type External Contribution Version Type publisher Keywords Astrodynamics · Orbital maneuvers · Thetered maneuvers · Escape trajectories Abstract The main idea of this paper is to propose the construction of an Escape Portal to send a spacecraft to the exterior planets, or even to make it escape from the Solar System, using a Tethered Sling Shot Maneuver (TSSM) with an asteroid. The construction of this portal allows an unlimited number of maneuvers with the same tether, which is very interesting when considering a possible use for small satellites. This structure would be formed by a tether that remains fixed in an asteroid. At the other end of the tether, a large net is fixed, such that the only action required from the spacecraft to make the TSSM is to hit the net. The net can have a mechanism to open a passage to release the spacecraft when the desired rotation is obtained. This technique would avoid some of the problems that appear when assuming that the spacecraft needs to carry a tether on board that would be released to hit the asteroid just before the maneuver. Area ETES Arrangement urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Building an “Escape... doc Directory Content access source Directory Content there are no files agreement Directory Content agreement.html 19/11/2018 14:07 1.0 KiB  4. Conditions of access and use Language en User Group self-uploading-INPE-MCTI-GOV-BR simone Visibility shown Archiving Policy denypublisher denyfinaldraft Read Permission deny from all and allow from 150.163 Update Permission not transferred 5. Allied materials Linking Trabalho não Vinculado à Tese/Dissertação Next Higher Units 8JMKD3MGPCW/446AF4B Dissemination WEBSCI; SCOPUS. Host Collection urlib.net/www/2017/11.22.19.04 6. Notes Empty Fields alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject targetfile tertiarytype url 7. Description control e-Mail (login) simone update

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