Fundamentals of Electric Propulsion Ion and Hall Thrusters

by ;
Edition: 1st
Format: Hardcover
Pub. Date: 2008-11-10
Publisher(s): Wiley
  • Free Shipping Icon

    This Item Qualifies for Free Shipping!*

    *Excludes marketplace orders.

List Price: $200.42

Buy New

Arriving Soon. Will ship when available.
$190.88

Rent Textbook

Select for Price
There was a problem. Please try again later.

Used Textbook

We're Sorry
Sold Out

eTextbook

We're Sorry
Not Available

How Marketplace Works:

  • This item is offered by an independent seller and not shipped from our warehouse
  • Item details like edition and cover design may differ from our description; see seller's comments before ordering.
  • Sellers much confirm and ship within two business days; otherwise, the order will be cancelled and refunded.
  • Marketplace purchases cannot be returned to eCampus.com. Contact the seller directly for inquiries; if no response within two days, contact customer service.
  • Additional shipping costs apply to Marketplace purchases. Review shipping costs at checkout.

Summary

This important new book explains the fundamentals of electric propulsion for spacecraft and describes in detail the physics and characteristics of the two major electric thrusters in use today, ion and Hall thrusters. The authors provide an introduction to plasma physics in order to allow readers to understand the models and derivations used in determining electric thruster performance. Next, they present detailed explanations of: thruster principles; ion thruster plasma generators and accelerator grids; hollow cathodes; hall thrusters; ion and Hall thruster plumes; and flight ion and Hall thrusters.

Author Biography

Dan M. Goebel, PhD, is a Senior Research Scientist in the Advanced Propulsion Technology Group at JPL in Pasadena, California. Since joining JPL in 2003, he has worked on the development of high-efficiency ion thrusters, advanced long life cathodes and grids, and electric-thruster life models for deep space missions. He is a world-recognized expert in ion thrusters, cathodes, advanced plasma sources, microwave sources, high-voltage engineering, and pulsed power switches.?

Ira Katz, PhD, has led the Advanced Propulsion Technology Group at NASA JPL since 2001. Group accomplishments during his tenure include the development and testing of the 25 kW NEXIS ion thruster, successful completion of the world's longest electric thruster life test, development of technology and support for precision formation flying missions (ST7, Lisa, TPF-I), and laboratory investigations and computer modeling of fundamental electric propulsion physics. Dr. Katz is recognized as a world leader in computer modeling of spacecraft-plasma interactions, spacecraft charging, and ion thruster physics.

Table of Contents

Note from the Series Editorp. ix
Forewordp. xi
Prefacep. xiii
Acknowledgmentsp. xv
Introductionp. 1
Electric Propulsion Backgroundp. 2
Electric Thruster Typesp. 3
Ion Thruster Geometryp. 6
Hall Thruster Geometryp. 6
Beam/Plume Characteristicsp. 9
Referencesp. 11
Thruster Principlesp. 15
The Rocket Equationp. 15
Force Transfer in Ion and Hall Thrustersp. 18
Thrustp. 21
Specific Impulsep. 25
Thruster Efficiencyp. 27
Power Dissipationp. 30
Neutral Densities and Ingestion in Electric Thrustersp. 32
Referencesp. 34
Problemsp. 35
Basic Plasma Physicsp. 37
Introductionp. 37
Maxwell's Equationsp. 38
Single Particle Motionsp. 39
Particle Energies and Velocitiesp. 43
Plasma as a Fluidp. 46
Momentum Conservationp. 46
Particle Conservationp. 48
Energy Conservationp. 51
Diffusion in Partially Ionized Gasesp. 54
Collisionsp. 55
Diffusion and Mobility Without a Magnetic Fieldp. 60
Diffusion Across Magnetic Fieldsp. 66
Sheaths at the Boundaries of Plasmasp. 71
Debye Sheathsp. 73
Pre-Sheathsp. 76
Child-Langmuir Sheathsp. 79
Generalized Sheath Solutionp. 81
Double Sheathsp. 84
Summary of Sheath Effectsp. 86
Referencesp. 88
Problemsp. 89
Ion Thruster Plasma Generatorsp. 91
Introductionp. 91
Idealized Ion Thruster Plasma Generatorp. 93
DC Discharge Ion Thrusterp. 100
Generalized 0-D Ring-Cusp Ion Thruster Modelp. 102
Magnetic Multipole Boundariesp. 105
Electron Confinementp. 108
Ion Confinement at the Anode Wallp. 110
Ion and Excited Neutral Productionp. 117
Neutral and Primary Densities in the Discharge Chamberp. 120
Power and Energy Balance in the Discharge Chamberp. 124
Discharge Lossp. 126
Discharge Stabilityp. 133
Recycling Behaviorp. 137
Limitations of a 0-D Modelp. 141
Kaufman Ion Thrustersp. 142
rf Ion Thrustersp. 148
Microwave Ion Thrustersp. 158
2-D Computer Models of the Ion Thruster Discharge Chamberp. 171
Neutral Atom Modelp. 172
Primary Electron Motion and Ionization Modelp. 176
Discharge Chamber Model Resultsp. 179
Referencesp. 182
Problemsp. 187
Ion Thruster Accelerator Gridsp. 189
Grid Configurationsp. 190
Ion Accelerator Basicsp. 196
Ion Opticsp. 200
Ion Trajectoriesp. 200
Perveance Limitsp. 204
Grid Expansion and Alignmentp. 206
Electron Backstreamingp. 208
High-Voltage Considerationsp. 216
Electrode Breakdownp. 217
Molybdenum Electrodesp. 218
Carbon-Carbon Composite Materialsp. 221
Pyrolytic Graphitep. 223
Hold-off and Conditioning in Ion Thrustersp. 224
Ion Accelerator Grid Lifep. 225
Grid Modelsp. 227
Barrel Erosionp. 230
Pits-and-Grooves Erosionp. 232
Referencesp. 235
Problemsp. 240
Hollow Cathodesp. 243
Introductionp. 243
Cathode Configurationsp. 248
Thermionic Electron Emitter Characteristicsp. 251
Insert Region Plasmap. 256
Orifice Region Plasmap. 270
Hollow Cathode Thermal Modelsp. 281
Cathode Plume-Region Plasmap. 283
Hollow Cathode Lifep. 292
Dispenser Cathodes in Insert Plasmasp. 293
Cathode Insert Temperaturep. 296
Barium Depletion Modelp. 298
Bulk-Material Insert Lifep. 302
Cathode Poisoningp. 304
Keeper Wear and Lifep. 306
Hollow Cathode Operationp. 309
Referencesp. 315
Problemsp. 321
Hall Thrustersp. 325
Introductionp. 325
Thruster Operating Principles and Scalingp. 329
Crossed-Field Structure and the Hall Currentp. 330
Ionization Length and Scalingp. 334
Potential and Current Distributionsp. 337
Hall Thruster Performance Modelsp. 341
Hall Thruster Efficiencyp. 341
Multiply Charged Ion Correctionp. 345
Dominant Power Loss Mechanismsp. 347
Plasma Electron Temperaturep. 357
Hall Thruster Efficiency (Dielectric Walls)p. 359
TAL Hall Thruster Efficiency (Metallic Walls)p. 363
Dielectric-Wall Versus Metallic-Wall Comparisonp. 364
Channel Physics and Numerical Modelingp. 365
Hybrid Hall Thruster Modelsp. 366
Steady-State Modeling Resultsp. 372
Oscillations in Hall Thrustersp. 376
Hall Thruster Lifep. 379
Referencesp. 384
Problemsp. 389
Ion and Hall Thruster Plumesp. 393
Introductionp. 393
Plume Physicsp. 395
Plume Measurementsp. 395
Flight Datap. 396
Laboratory Plume Measurementsp. 398
Plume Modelsp. 400
Primary Beam Expansionp. 400
Neutral Gas Plumesp. 407
Secondary-Ion Generationp. 408
Spacecraft Interactionsp. 410
Momentum of the Plume Particlesp. 412
Sputtering and Contaminationp. 413
Plasma Interactions with Solar Arraysp. 415
Interactions with Payloadsp. 418
Microwave Phase Shiftp. 418
Plume Plasma Optical Emissionp. 419
Referencesp. 422
Problemsp. 424
Flight Ion and Hall Thrustersp. 429
Introductionp. 429
Ion Thrustersp. 429
Hall Thrustersp. 440
Referencesp. 443
Appendices
Nomenclaturep. 447
Gas Flow Unit Conversions and Cathode Pressure Estimatesp. 463
Energy Loss by Electronsp. 467
Ionization and Excitation Cross Sections for Xenonp. 471
Ionization and Excitation Reaction Rates for Xenon in Maxwellian Plasmasp. 475
Electron Relaxation and Thermalization Timesp. 479
Clausing Factor Monte Carlo Calculationp. 483
Indexp. 487
Table of Contents provided by Ingram. All Rights Reserved.

An electronic version of this book is available through VitalSource.

This book is viewable on PC, Mac, iPhone, iPad, iPod Touch, and most smartphones.

By purchasing, you will be able to view this book online, as well as download it, for the chosen number of days.

Digital License

You are licensing a digital product for a set duration. Durations are set forth in the product description, with "Lifetime" typically meaning five (5) years of online access and permanent download to a supported device. All licenses are non-transferable.

More details can be found here.

A downloadable version of this book is available through the eCampus Reader or compatible Adobe readers.

Applications are available on iOS, Android, PC, Mac, and Windows Mobile platforms.

Please view the compatibility matrix prior to purchase.