Building an “Escape Portal” with Tethers Fixed in Asteroids
dc.contributor.author | Prado, Antonio F. B. A. | |
dc.contributor.author | Gomes, Vivian Martins [UNESP] | |
dc.contributor.author | Chanut, Thierry Gregory Gil [UNESP] | |
dc.contributor.institution | INPE | |
dc.contributor.institution | Universidade Estadual Paulista (Unesp) | |
dc.date.accessioned | 2019-10-06T16:54:23Z | |
dc.date.available | 2019-10-06T16:54:23Z | |
dc.date.issued | 2018-09-15 | |
dc.description.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. | en |
dc.description.affiliation | INPE, Av dos Astronautas 1758 | |
dc.description.affiliation | Unesp Universidade Estadual Paulista | |
dc.description.affiliationUnesp | Unesp Universidade Estadual Paulista | |
dc.description.sponsorship | Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP) | |
dc.description.sponsorship | Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq) | |
dc.description.sponsorshipId | FAPESP: 2011/13101-4 | |
dc.description.sponsorshipId | FAPESP: 2016/14665-2 | |
dc.description.sponsorshipId | FAPESP: 2016/24561-0 | |
dc.description.sponsorshipId | CNPq: 301338/2016-7 | |
dc.description.sponsorshipId | CNPq: 406841/2016-0 | |
dc.format.extent | 355-375 | |
dc.identifier | http://dx.doi.org/10.1007/s40295-017-0120-x | |
dc.identifier.citation | Journal of the Astronautical Sciences, v. 65, n. 3, p. 355-375, 2018. | |
dc.identifier.doi | 10.1007/s40295-017-0120-x | |
dc.identifier.issn | 2195-0571 | |
dc.identifier.issn | 0021-9142 | |
dc.identifier.scopus | 2-s2.0-85056076871 | |
dc.identifier.uri | http://hdl.handle.net/11449/189857 | |
dc.language.iso | eng | |
dc.relation.ispartof | Journal of the Astronautical Sciences | |
dc.rights.accessRights | Acesso restrito | |
dc.source | Scopus | |
dc.subject | Astrodynamics | |
dc.subject | Escape trajectories | |
dc.subject | Orbital maneuvers | |
dc.subject | Thetered maneuvers | |
dc.title | Building an “Escape Portal” with Tethers Fixed in Asteroids | en |
dc.type | Artigo | |
unesp.department | Matemática - FEG | pt |