Memorias de investigación
Capítulo de libro:
BETs: Propellantless deorbiting of space debris by bare electrodynamic tethers
Año:2012

Áreas de investigación
  • Fisica y ciencias del espacio

Datos
Descripción
As a fundamental contribution to limiting the increase of debris in the Space environment, a three-year project started on 1 November 2010 financed by the European Commission under the FP-7 Space Programme. It aims at developing a universal system to be carried on board future satellites launched into low Earth orbit (LEO), to allow de-orbiting at end of life. The operational system involves a conductive tape-tether left bare of insulation to establish anodic contact with the ambient plasma as a giant Langmuir probe. The project will size the three disparate dimensions of a tape for a selected de-orbit mission and determine scaling laws to allow system design for a general mission. It will implement control laws to restrain tether dynamics inl off the orbital plane; and will carry out plasma chamber measurements and numerical simulations of tether-plasma interaction. The project also involves the design and manufacturing of subsystems: electron-ejecting plasma contactors, an electric control and power module, interface elements, tether and deployment mechanisms, tether tapel end-mass as well as current collection plus free-fall, and hypervelocity impact tests.
Internacional
Si
DOI
10.2769/31208
Edición del Libro
Editorial del Libro
European Union, 2012
ISBN
978-92-79-22207-8
Serie
Título del Libro
Let's embrace space, Vol. II
Desde página
506
Hasta página
513

Esta actividad pertenece a memorias de investigación

Participantes
  • Autor: Juan Ramon Sanmartin Losada UPM
  • Autor: Mario Charro Cubero UPM
  • Autor: et al.

Grupos de investigación, Departamentos, Centros e Institutos de I+D+i relacionados
  • Creador: Grupo de Investigación: Grupo de Investigación en Fusión Inercial y Física de Plasmas
  • Departamento: Física Aplicada a la Ingeniería Aeronáutica