Method for Analyzing ExB Probe Spectra from Hall Thruster Plumes

Method for Analyzing ExB Probe Spectra from Hall Thruster Plumes

著者名:

R. Shastry ( Jet Propulsion Laboratory California Institute of Technology, Pasadena, CA )
R. Hofer
B. Reid ( The University of Michigan, Ann Arbor, MI )
A. Gallimore

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

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

シリーズ巻号:

2008

発行年:

2008

通号:

2008-4647

ペーパー番号:

AIAA 2008-4647

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200808 [CD-ROM 2008 Disc 8]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050885
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
回次:	44th
会議開催地:	Hartford, CT
会議開催年:	2008.07.21-2008.07.23
論文注記:	44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, 21-23 July 2008

類似資料:

1 テクニカルペーパー Angularly-Resolved ExB Probe Spectra in the Plume of a 6-kW Hall Thruster B. Reid, R. Shastry, A. Gallimore, R. Hofer American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Efficiency Analysis of a High-Specific Impulse Hall Thruster Hofer, R., Gallimore, A. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Efficiency Analysis of a Low Discharge Voltage Hall Thruster R. Shastry, A. Gallimore, R. Hofer American Institute of Aeronautics and Astronautics	8 テクニカルペーパー 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 テクニカルペーパー Langmuir Probe Measurements in the Discharge Channel of a 6-kW Hall Thruster B. Reid, A. Gallimore American Institute of Aeronautics and Astronautics	9 テクニカルペーパー 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
4 テクニカルペーパー 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	10 テクニカルペーパー Plasma Potential Measurements in the Discharge Channel of a 6-kW Hall Thruster B. Reid, A. Gallimore American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Ion Species Fractions in the Far-Field Plume of a High-Specific Impulse Hall Thruster Hofer, R.R., Gallimore, A.D. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー 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
6 テクニカルペーパー Laser-Induced Fluorescence of Singly-Charged Xenon in a 6-kW Hall Thruster Plume W. Huang, B. Reid, T. Smith, A. Gallimore American Institute of Aeronautics and Astronautics	12 テクニカルペーパー 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

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