Inertial Electrostatic Confinement Thruster (IECT)
eBook - PDF

Inertial Electrostatic Confinement Thruster (IECT)

Development, Modeling, and Characterization

  1. 273 pages
  2. English
  3. PDF
  4. Available on iOS & Android
eBook - PDF

Inertial Electrostatic Confinement Thruster (IECT)

Development, Modeling, and Characterization

About this book

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.

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Information

Year
2022
Print ISBN
9783736976771
eBook ISBN
9783736966772
Edition
1

Table of contents

  1. Acknowledgment
  2. Abstract
  3. Zusammenfassung
  4. Contents
  5. Nomenclature
  6. Chapter 1 Introduction
  7. 1.1 Background of Inertial Electrostatic Confinement
  8. 1.2 Magnetic Nozzle for IEC Plasma Acceleration
  9. 1.3 Potential Applications
  10. 1.4 Motivation and Difficulties
  11. 1.5 Thesis Structure
  12. Chapter 2 Fundamentals of DC Discharge and IEC Theory
  13. 2.1 Fundamentals of DC Plasma Discharge
  14. 2.2 The New Perspective of the IEC Working Principle
  15. 2.3 Implementation of the IEC-SDL Model
  16. 2.4 Summary of IEC Discharge Theory
  17. Chapter 3 Plasma Acceleration in Magnetic Nozzle
  18. 3.1 Summary of the Plasma Transportation and MHD Flow Theory
  19. 3.2 Plasma Acceleration in a Divergent B-field
  20. 3.3 Plasma Detachment Mechanism
  21. 3.4 Design Criteria of MN for IEC Plasma Source
  22. Chapter 4 IECT Design and Test Facility
  23. 4.1 The Design Concept and Considerations of IECT
  24. 4.2 Phase I: IEC Discharge Experiment
  25. 4.3 Phase II: IECT Experiment
  26. 4.4 IECT Test Facility
  27. Chapter 5 Plasma Diagnostics for IEC Plasma Sphere
  28. 5.1 Narrow Spectral-bandwidth Imaging
  29. 5.2 Optical Emission Spectroscopy
  30. 5.3 Collisional Radiative Model
  31. Chapter 6 Plasma Diagnostics for IECT Plume
  32. 6.1 Principle of the Electrostatic Probe
  33. 6.2 Probe Design and Experimental Setup
  34. Chapter 7 Discharge Evaluation of IEC Plasma Source
  35. 7.1 Discharge Behavior of IEC Plasma Source
  36. 7.2 SDL Characteristics
  37. 7.3 Conclusions of IEC Discharge Experiment
  38. Chapter 8 EMN Discharge and Plume Characteristics
  39. 8.1 EMN Discharge Characteristics
  40. 8.2 IECT Plume Properties
  41. 8.3 Summary of EMN Discharge Characteristics and Plume Properties
  42. Chapter 9 Conclusion
  43. 9.1 Discharge of IEC and SDL Theory
  44. 9.2 Plasma Confinement and Acceleration by EMN
  45. Bibliography
  46. Appendix