Ion Current Density Study of the NASA-300M and NASA-457Mv2 Hall Thrusters-Reference-Cited by-同舟云学术

Ion Current Density Study of the NASA-300M and NASA-457Mv2 Hall Thrusters

Published:2012-07-30 Issue: Volume: Page:
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Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Huang Wensheng,Shastry Rohit,Herman Daniel,Soulas George,Kamhawi Hani

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. 2Mercer, C. R. "Benefits of Power and Propulsion Technology for a Piloted Electric Vehicle to an Asteroid ", 47th AIAA/ASME/SAE/ASEEJointPropulsion Conference &Exhibit,AIAA-2011-7252, SanDiego,CA, 31 Jul. 3Aug.,2011.

2. 3Capadona, L. A. "Feasibility of Large High-Powered Solar Electric Propulsion Vehicles: Issues and Solutions", 47th AIAA/ASME/SAE/ASEEJointPropulsion Conference &Exhibit,AIAA-2011-7251, SanDiego,CA, 31 Jul. 3Aug.,2011.

3. 5Hofer, R. R. and Randolph, T. M. "Mass and Cost Model for Selecting Thruster Size in Electric Propulsion Systems", 47th AIAA/ASME/SAE/ASEEJointPropulsion Conference &Exhibit,AIAA-2011-5518, SanDiego,CA, 31 Jul. 3Aug.,2011.

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5. Plasma Potential and Langmuir Probe Measurements in the Near-field Plume of the NASA-300M Hall Thruster;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30