Resumen
A 3-year Project started on November 1 2010, financed by the European Commision within the FP-7 Space Program, and aimed at developing an efficient de-orbit system that could be carried on board by future spacecraft launched into LEO, will be presented. The operational system will deploy a thin uninsulated tape-tether to collect electrons as a giant Langmuir probe, using no propellant/no power supply, and generating power on board. This project will involve free-fall tests, and laboratory hypervelocity-impact and tether-current tests, and design/Manufacturing of subsystems: interface elements, electric control and driving module, electron-ejecting plasma contactor, tether-deployment mechanism/end-mass, and tape samples. Preliminary results to be presented involve: i) devising criteria for sizing the three disparate tape dimensions, affecting mass, resistance, current-collection, magnetic self-field, and survivability against debris itself; ii) assessing the dynamical relevance of tether parameters in implementing control laws to limit oscillations in /off the orbital plane, where passive stability may be marginal; iii) deriving a law for bare-tape current from numerical simulations and chamber tests, taking into account ambient magnetic field, ion ram motion, and adiabatic electron trapping; iv) determining requirements on a year-dormant hollow cathode under long times/broad emission-range operation, and trading-off against use of electron thermal emission; v) determining requirements on magnetic components and power semiconductors for a control module that faces high voltage/power operation under mass/volume limitations; vi) assessing strategies to passively deploy a wide conductive tape that needs no retrieval, while avoiding jamming and ending at minimum libration; vii) evaluating the tape structure as regards conductive and dielectric materials, both lengthwise and in its cross-section, in particular to prevent arcing in triple-point junctions.
| Idioma original | Inglés |
|---|---|
| Título de la publicación alojada | 62nd International Astronautical Congress 2011, IAC 2011 |
| Páginas | 2239-2248 |
| Número de páginas | 10 |
| Estado | Publicada - 2011 |
| Evento | 62nd International Astronautical Congress 2011, IAC 2011 - Cape Town, Sudáfrica Duración: 3 oct 2011 → 7 oct 2011 |
Serie de la publicación
| Nombre | 62nd International Astronautical Congress 2011, IAC 2011 |
|---|---|
| Volumen | 3 |
Conferencia
| Conferencia | 62nd International Astronautical Congress 2011, IAC 2011 |
|---|---|
| País/Territorio | Sudáfrica |
| Ciudad | Cape Town |
| Período | 3/10/11 → 7/10/11 |
ODS de las Naciones Unidas
Este resultado contribuye a los siguientes Objetivos de Desarrollo Sostenible
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ODS 9: Industria, innovación e infraestructura
Huella
Profundice en los temas de investigación de 'Propellantless deorbiting of space debris by bare electrodynamic tethers'. En conjunto forman una huella única.Citar esto
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