Thrust measurements and mesothermal plasma plume of the Alternative Low Power Hybrid Ion Engine (alphie)

Conde López, Luis ORCID: https://orcid.org/0000-0002-3830-9439, González Muñoz, Jorge ORCID: https://orcid.org/0000-0001-7905-5001, Donoso Vargas, Jose Manuel ORCID: https://orcid.org/0000-0002-5532-0648, Domenech Garret, Juan Luis ORCID: https://orcid.org/0000-0001-8137-1345 and Castillo, M.A. (2022). Thrust measurements and mesothermal plasma plume of the Alternative Low Power Hybrid Ion Engine (alphie). "Journal of Electric Propulsion", v. 1 ; p. 24. ISSN 27314596. https://doi.org/10.1007/s44205-022-00027-6.

Descripción

Título: Thrust measurements and mesothermal plasma plume of the Alternative Low Power Hybrid Ion Engine (alphie)
Autor/es:
Tipo de Documento: Artículo
Título de Revista/Publicación: Journal of Electric Propulsion
Fecha: 14 Noviembre 2022
ISSN: 27314596
Volumen: 1
Materias:
ODS:
Palabras Clave Informales: Affordable and clean energy; Ion engine; Ion velocity distribution; Plasma plume; Specific impulse
Escuela: E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM)
Departamento: Física Aplicada a las Ingenierías Aeronáutica y Naval
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

Texto completo

[thumbnail of 10429583.pdf] PDF (Portable Document Format) - Se necesita un visor de ficheros PDF, como GSview, Xpdf o Adobe Acrobat Reader
Descargar (2MB)

Resumen

The high specific impulse Alternative Low Power Ion Engine (alphie) is a gridded plasma thruster different from conventional (Kaufman) ion engines. In this disruptive concept, the ionization of the propellant neutral gas and the neutralization of ion outflow is achieved with only one cathode located in front and outside of the thruster. Electrons and ions move under the self-consistent field created by the DC voltage applied to its two planar grids together with the currents of charges flowing through them, unlike to conventional ion engines, where only ions move through its ion optics system. The stationary mesothermal flow of ions and electrons in the plasma plume is characterized with a retarded field energy analyzer in conjunction with Langmuir and emissive probes. The ion velocity distribution functions and the electron energy spectra for different operating conditions of the alphie thruster are discussed. The observed high ion temperatures are explained by the collisional interaction between the fast ionizing electrons and the neutral atoms that increases their average kinetic energy. Finally, the alphie delivers 0.8-3.5 mN throttleable thrusts giving specific impulses in the range of 14000-20000 s with estimated thruster efficiencies between 8% and 40%.

Proyectos asociados

Tipo
Código
Acrónimo
Responsable
Título
Gobierno de España
RT2018-094409-B-100.
Sin especificar
Sin especificar
Sin especificar

Más información

ID de Registro: 92897
Identificador DC: https://oa.upm.es/92897/
Identificador OAI: oai:oa.upm.es:92897
URL Portal Científico: https://portalcientifico.upm.es/es/ipublic/item/10429583
Identificador DOI: 10.1007/s44205-022-00027-6
URL Oficial: https://link.springer.com/article/10.1007/s44205-0...
Depositado por: iMarina Portal Científico
Depositado el: 15 Ene 2026 08:31
Ultima Modificación: 15 Ene 2026 08:31