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Short, high current electrodynamic tether
Cita
Savich, N.A. and Sanmartín Losada, Juan Ramón
(1994).
Short, high current electrodynamic tether.
En: "International Round Table on Tethers in Space", 28-30 sept, Noordwijk.
Descripción
| Título: | Short, high current electrodynamic tether |
|---|---|
| Autor/es: |
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| Tipo de Documento: | Ponencia en Congreso o Jornada (Artículo) |
| Título del Evento: | International Round Table on Tethers in Space |
| Fechas del Evento: | 28-30 sept |
| Lugar del Evento: | Noordwijk |
| Título del Libro: | Proceedings of the International Round Table on Tethers in Space |
| Fecha: | 1994 |
| Materias: | |
| ODS: | |
| Escuela: | E.T.S.I. Aeronáuticos (UPM) [antigua denominación] |
| Departamento: | Física Aplicada a la Ingeniería Aeronáutica [hasta 2014] |
| Licencias Creative Commons: | Reconocimiento - Sin obra derivada - No comercial |
Resumen
An electrodynamic tether experiment, to be carried out in the Russian spacecraft Almaz, is proposed. A 10 km tether would be deployed downwards; the lower 8 km would be nonconductive, the upper 2 km would be conductive, bare, and 2.2 mm in diameter, and would act as a thruster, with power supply at the top. This hybrid arrangement allows for other, onelectrodynamic experiments,reducing costs; it also limits the induced electromotive force, reducing the power to be handled. The current-voltage characteristic of contactors would be measured. With the anode switched off, the wire itself should collect a current over 5 A at day conditions, providing a thrust of 0.11 N at a 0.77 kW power.
Más información
| ID de Registro: | 23412 |
|---|---|
| Identificador DC: | https://oa.upm.es/23412/ |
| Identificador OAI: | oai:oa.upm.es:23412 |
| Depositado por: | Biblioteca ETSI Aeronauticos |
| Depositado el: | 09 Abr 2014 07:40 |
| Ultima Modificación: | 15 Feb 2023 07:35 |
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