%0 Journal Article
%@nexthigherunit 8JMKD3MGPCW/446AF4B
%@holdercode {isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}
%@secondarymark B1_CIÊNCIAS_AGRÁRIAS A2_ENGENHARIAS_I B2_ENGENHARIAS_II B1_ENGENHARIAS_III B2_ENGENHARIAS_IV B1_INTERDISCIPLINAR B1_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA
%@mirrorrepository sid.inpe.br/mtc-m19@80/2009/08.21.17.02.53
%D 2009
%4 sid.inpe.br/mtc-m19@80/2009/12.17.14.00
%T Analysis of electric propulsion system for exploration of Saturn
%@usergroup administrator
%@usergroup banon
%@usergroup marciana
%U 1024-123X
%V 2009
%@affiliation Instituto Nacional de Pesquisas Espaciais (INPE)
%@affiliation Instituto Nacional de Pesquisas Espaciais (INPE)
%@affiliation IKI, Space Res Inst, Flight Dynam & Data Proc Div, Moscow 117997, Russia
%@project FAPESP [(2008/10236-3), (2007/04232-2)]
%@versiontype publisher
%X ABSTRACT: Exploration of the outer planets has experienced new interest with the launch of the Cassini and the New Horizons Missions. At the present time, new technologies are under study for the better use of electric propulsion system in deep space missions. In the present paper, the method of the transporting trajectory is used to study this problem. This approximated method for the flight optimization with power-limited low thrust is based on the linearization of the motion of a spacecraft near a keplerian orbit that is close to the transfer trajectory. With the goal of maximizing the mass to be delivered in Saturn, several transfers were studied using nuclear, radioisotopic and solar electric propulsion systems.
%@area ETES
%@secondarykey INPE--PRE/
%@documentstage not transferred
%K electric propulsion system, space missions, Saturn.
%@archivingpolicy denypublisher allowfinaldraft
%@doi 10.1155/2009/756037
%@issn 1024-123X
%@issn 1563-5147
%@group DMC-ETE-INPE-MCT-BR
%@group DMC-ETE-INPE-MCT-BR
%@dissemination WEBSCI
%P 14 pp
%A Solorzano, Carlos Renato Huaura,
%A Prado, Antonio Fernando Bertachini de Almeida,
%A Sukhanov, Alexander Alexandrovich,
%B Mathematical Problems in Engineering
%2 sid.inpe.br/mtc-m19@80/2009/12.17.14.00.56
%@secondarytype PRE PI