EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT
@inproceedings{Hopkins2015EVALUATIONOM, title={EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT}, author={Mark A. Hopkins}, year={2015} }
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Effect of Channel Shape on Hall thruster Performance Using Argon and Xenon propellant
- Engineering
- 2019
Recently, alternative propellant is required because xenon price is increasing yearly. Argon which is the cheapest gas to use EPs, have not been a strong candidate because of its poor performance.…
References
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The feasibility of using magnesium (Mg) and zinc (Zn) vapor as Hall Effect Thruster propellant was proven. Mg and Zn are plentiful, non-toxic, low cost alternatives to xenon and krypton. Because Zn…
Internal plasma potential measurements of a Hall thruster using xenon and krypton propellant (10 pages)
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For krypton to become a realistic option for Hall thruster operation, it is necessary to understand the performance gap between xenon and krypton and what can be done to reduce it. A floating…
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§This paper describes what are believed to be the first demonstrations of Hall-effect thrusters operating on magnesium and zinc propellant. Pathfinding experiments were performed using consumable…
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The effects of anode temperature on the performance of a 5-kW Hall-effect thruster are investigated. The performance characteristics of the P5 Hall-effect thruster are measured with and without…
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The performance of a nominal 200 W Hall effect thruster fueled by iodine vapor was evaluated. The system included a laboratory propellant feed system, a flight-model Hall thruster, and breadboard…
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A thrust stand for use with magnetoplasmadynamic (MPD) thrusters operated at powers up to 250 kW steady state has been built and tested. The stand was based on an inverted pendulum configuration…
Characterizing Vacuum Facility Backpressure Effects on the Performance of a Hall Thruster
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* Presented as Paper IEPC-01-045 at the 27 International Electric Propulsion Conference, Pasadena, CA, 15-19 October 2001. † Copyright © 2001 by the Electric Rocket Propulsion Society. All rights…
Development and Testing of a Prototype Bismuth Cathode for Hall Thrusters
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- 2005
Using bismuth in place of gases such as xenon for Hall thruster propellant could potentially offer both physical and economical gains. As research continues to develop Hall thrusters that are fueled…
Progress on the Development of a Direct Evaporation Bismuth Hall Thruster
- Engineering
- 2005
It has been demonstrated that using segmented anodes for thermal regulation of anodes is possible by controlling where the discharge current attaches to. Thrust, Isp and efficiency measurements were…
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- 2014
We demonstrate a technique by which erosion of the acceleration channel in Hall thrusters can be reduced by at least a few orders of magnitude. The first principles of the technique, now known as…