Considerations on the Role of the Hall Current in a Laboratory-Model Thruster

Considerations on the Role of the Hall Current in a Laboratory-Model Thruster

Author(s):

Haas,J.M. ( Plasmadynamics and Electric Propulsion Laboratory Department of Aerospace Engineering The University of Michigan )
Gallimore,A.D.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-3507

Paper no.:

AIAA-2001-3507

Page(from):

1

Page(to):

14

Pages:

14

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050826
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC) & Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Salt Lake City, UT
Conf. info. (Date):	2001.07.08-2001.07.11
Note for article:	37th Joint Propulsion Conference & Exhibit 8-11 July 2001 Salt Lake City, Utah

Similar Items:

1 Technical Paper Ion Voltage Diagnostics in the Far-Field Plume of a High-Specific Impulse Hall Thruster Hofer, R.R., Haas, J.M., Gallimore, A.D. American Institute of Aeronautics and Astronautics	7 Technical Paper Hall Thruster Discharge Chamber Plasma Characterization Using a High-Speed Axial Reciprocating Electrostatic Probe Haas, James M., Hofer, Richard R., Gallimore, Alec D. American Institute of Aeronautics and Astronautics
2 Technical Paper An Investigation of Internal Ion Number Density and Electron Temperature Profiles in a Laboratory-Model Hall Thruster Haas, James M., Gallimore, Alec D. American Institute of Aeronautics and Astronautics	8 Technical Paper Hall thruster discharge chamber plasma characterization using a high-speed axial reciprocating electrostatic probe Haas, James M., Hofer, Richard R., Gallimore, Alec D. American Institute of Aeronautics and Astronautics
3 Technical Paper Performance characteristics of a 5 kW laboratory hall thruster Haas, James M., Gulczinski, Frank S., Gallimore, Alec D., Spanjers, Gregory G., Spores, Ronald A. American Institute of Aeronautics and Astronautics	9 Technical Paper Parametric investigation of orifice aspect-ratio effects on low-current hollow cathode power consumption Domonkos, M.T., Gallimore, A.D., Patterson, M.J. American Institute of Aeronautics and Astronautics
4 Technical Paper The Role of Magnetic Field Topography in Improving the Performance of High-Voltage Hall Thrusters. Hofer, R.R., Gallimore, A.D. American Institute of Aeronautics and Astronautics	10 Technical Paper COMPUTATION OF THE INTERIOR AND NEAR-FIELD FLOW OF A 2-kW CLASS HALL THRUSTER Koo,Justin W., Boyd,Iain D., Haas,James M., Gallimore,Alec D. American Institute of Aeronautics and Astronautics
5 Technical Paper The Effects of Nude Faraday Probe Design and Vacuum Facility Backpressure on the Measured Ion Current Density Profile of Hall Thruster Plumes. Walker, M.L.R., Hofer, R.R., Gallimore, A.D. American Institute of Aeronautics and Astronautics	11 Technical Paper Evaluation of a Magnetically Filtered Faraday Probe for Measuring the Ion Current Density Profile of a Hall Thruster Rovey, J., Walker, M., Peterson, P., Gallimore, A. American Institute of Aeronautics and Astronautics
6 Technical Paper EXPERIMENTAL INVESTIGATION OF HALL THRUSTER INTERAL MAGNETIC FIELD TOPOGRAPHY Peterson,Peter Y., Gallimore,Alec D., Haas,James M. American Institute of Aeronautics and Astronautics	12 Technical Paper Performance Characteristics of a Cluster of 5 kW Laboratory Hall Thrusters Walker, M., Gallimore, A. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12