English   español  
Por favor, use este identificador para citar o enlazar a este item: http://hdl.handle.net/10261/8198
Compartir / Impacto:
Add this article to your Mendeley library MendeleyBASE
Citado 48 veces en Web of Knowledge®  |  Ver citas en Google académico
Visualizar otros formatos: MARC | Dublin Core | RDF | ORE | MODS | METS | DIDL
Exportar otros formatos: Exportar EndNote (RIS)Exportar EndNote (RIS)Exportar EndNote (RIS)
Título : TandEM: Titan and Enceladus mission
Autor : Coustenis, A.; López-Moreno, José Juan ; Ruiz Bermejo, Marta ; Menor-Salván, César ; Lara, Luisa María ; Martínez-Frías, J.; Young, Eliot Fisher; Nna Mvondo, Delphine ; Amils, Ricardo; Prieto-Ballesteros, Olga ; Rodrigo Montero, Rafael
Palabras clave : TandEM
Saturnian system
Landing probes
Fecha de publicación : 8-jul-2008
Editor: Springer
Citación : Experimental Astronomy 23(3): 893-946 (2008)
Resumen: TandEM was proposed as an L-class (large) mission in response to ESA’s Cosmic Vision 2015–2025 Call, and accepted for further studies, with the goal of exploring Titan and Enceladus. The mission concept is to perform in situ investigations of two worlds tied together by location and properties, whose remarkable natures have been partly revealed by the ongoing Cassini–Huygens mission. These bodies still hold mysteries requiring a complete exploration using a variety of vehicles and instruments. TandEM is an ambitious mission because its targets are two of the most exciting and challenging bodies in the Solar System. It is designed to build on but exceed the scientific and technological accomplishments of the Cassini–Huygens mission, exploring Titan and Enceladus in ways that are not currently possible (full close-up and in situ coverage over long periods of time). In the current mission architecture, TandEM proposes to deliver two medium-sized spacecraft to the Saturnian system. One spacecraft would be an orbiter with a large host of instruments which would perform several Enceladus flybys and deliver penetrators to its surface before going into a dedicated orbit around Titan alone, while the other spacecraft would carry the Titan in situ investigation components, i.e. a hot-air balloon (Montgolfière) and possibly several landing probes to be delivered through the atmosphere.
Descripción : 54 páginas, 8 figuras.-- Coustenis, A. et al.
Versión del editor: http://dx.doi.org/10.1007/s10686-008-9103-z
URI : http://hdl.handle.net/10261/8198
DOI: 10.1007/s10686-008-9103-z
ISSN: 0922-6435 (Print)
1572-9508 (Online)
Aparece en las colecciones: (CAB) Artículos
(IAA) Artículos
Ficheros en este ítem:
No hay ficheros asociados a este ítem.
Mostrar el registro completo

NOTA: Los ítems de Digital.CSIC están protegidos por copyright, con todos los derechos reservados, a menos que se indique lo contrario.