Inertial Electrostatic Confinement Thruster (IECT)
Development, Modeling, and Characterization
Seiten
2022
Cuvillier Verlag
978-3-7369-7677-1 (ISBN)
Cuvillier Verlag
978-3-7369-7677-1 (ISBN)
This work summarizes the state-of-the-art development of inertial electrostatic confinement (IEC) thruster, which can be divided into two parallel lines of development: the IEC plasma source and the corresponding electromagnetic nozzle (EMN). Both developing lines start from the establishment of the theory and modeling and evolve to the design implementation and experimental verification.
The IEC discharge model highlights a novel perspective on the IEC discharge physics and the impacts of the respective critical parameters, which layouts the design for the IEC plasma source. Experimental verification for the theory is demonstrated via the optical emission spectroscopy and collision radiative model. The results provide conclusive evidence of forming a spherical double layer within the IEC plasma source, which is the key to establishing the proposed IEC discharge theory in this work.
This work presents a comprehensive study on the magnetohydrodynamic theory for assessing the plasma acceleration in the magnetic nozzle. Nevertheless, the result shows a performance limitation of the magnetic nozzle. An innovative invention is proposed to overcome the limitation known as the EMN. Thorough descriptions of EMN and its working principle are summarized in this work, including its effects on plasma confinement, acceleration, and detachment. Investigation of the plasma plume properties by miscellaneous plasma diagnostics tools further demonstrates EMN functionality and constitutes the first IECT prototype with proof-of-concept in literature.
The IEC discharge model highlights a novel perspective on the IEC discharge physics and the impacts of the respective critical parameters, which layouts the design for the IEC plasma source. Experimental verification for the theory is demonstrated via the optical emission spectroscopy and collision radiative model. The results provide conclusive evidence of forming a spherical double layer within the IEC plasma source, which is the key to establishing the proposed IEC discharge theory in this work.
This work presents a comprehensive study on the magnetohydrodynamic theory for assessing the plasma acceleration in the magnetic nozzle. Nevertheless, the result shows a performance limitation of the magnetic nozzle. An innovative invention is proposed to overcome the limitation known as the EMN. Thorough descriptions of EMN and its working principle are summarized in this work, including its effects on plasma confinement, acceleration, and detachment. Investigation of the plasma plume properties by miscellaneous plasma diagnostics tools further demonstrates EMN functionality and constitutes the first IECT prototype with proof-of-concept in literature.
Erscheinungsdatum | 28.09.2022 |
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Verlagsort | Göttingen |
Sprache | englisch |
Maße | 148 x 210 mm |
Themenwelt | Technik ► Luft- / Raumfahrttechnik |
Technik ► Maschinenbau | |
Schlagworte | 3D-printing electrode, collisional radiative model • abgestumpftes Kuboktaeder • Bildgebung mit schmaler spektraler Bandbreite • BSSB • CRM, EEDF, EMN, EP, IEC, MHD • double layer, electron beam • EA • electric propulsion, electromagnetic nozzle • electron diamagnetic current, electron dynamics • electron energy distribution function • electron multiplication, electric potential topography • Elektrischer Antrieb • elektromagnetische Düse, Faraday-Sonde • Elektronendynamik • Elektronenenergieverteilungsfunktion • Elektronenstrahl, diamagnetischer Elektronenstrom • Elektronenvervielfachung • elektrostatischer Trägheitseinschluss, Langmuir-Sonde • Faraday probe, hollow cathode discharge • Hohlkathodenentladung • inertial electrostatic confinement, Langmuir probe • magnetic nozzle, magnetohydrodynamics • magnetische Düse • Magnetohydrodynamik • MD • MN, NBWI, OES • narrow spectral-bandwidth imaging • nicht-neutrales Plasma • non-neutral plasma, optical emission spectroscopy • Optische Emissionsspektroskopie • Plasma-Abtrennung • plasma acceleration, plasma confinement • Plasmabeschleunigung • Plasmabeschränkung • plasma detachment, plasma diagnostics • Plasmadiagnostik • Plasma discharge • Plasmaentladung • plasma extraction, plasma source, space propulsion • Plasmaextraktion • Plasmaquelle • Raumfahrtantrieb • SDL,3D gedruckte Elektrode • sphärische Doppelschicht • spherical double layer • SSM, EMD, • Stoß-Strahlungsmodelle, Doppelschicht • Topographie des elektrischen Potentials • truncated cuboctahedron |
ISBN-10 | 3-7369-7677-1 / 3736976771 |
ISBN-13 | 978-3-7369-7677-1 / 9783736976771 |
Zustand | Neuware |
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