THE DEVELOPMENT AND QUALIFICATION OF A 4.5 KW HALL THRUSTER PROPULSION SYSTEM
This paper provides an updated status of the 4.5 kW Hall Thruster Propulsion Subsystem development and qualification program at Aerojet’s Redmond operation (formerly General Dynamics Space Propulsion System) and Lockheed Martin. This subsystem is being developed to support geosynchronous satellite applications for both commercial and military applications. This paper describes the mission application, performance, program plan and current status of the development program. The overall system, including the Power Processor Unit, the Xenon Flowrate Controller, the Hall Thruster and Cathode and the Xenon Feed System is also described. The system currently under development is planned to be used for both orbit insertion from an initial geosynchronous transfer orbit and on-orbit stationkeeping and repositioning maneuvers. The HTPS takes advantage of the dual-mode capabilities and wide operating power range of the Aerojet BPT-4000 Hall thruster to maximize efficiency for each mission phase.
The Development and Qualification of a 4.5 kW Hall Thruster Propulsion System for GEO Satellite Applications
* Presented as Paper IEPC-01-010 at the 27 International Electric Propulsion Conference, Pasadena, CA, 15-19 October, 2001. † Copyright  2001 by General Dynamics SPS. Published by the Electric Rocket Propulsion Society with permission. This paper summarizes the current program at General Dynamics Space Propulsion Systems (formerly Primex Aerospace Company) and Lockheed Martin to develop and qualify a 4.5 kW Hall Thruster Propulsion Subsystem. This subsystem is being developed to support geo-synchronous satellite applications. This paper describes the mission application, performance, program plan and current status of the development program. The overall system, including the Power Processor Unit, the Xenon Flowrate Controller, the Hall Thruster and Cathode and the Xenon Feed System is also described.
Experimental Study on Acoustic Agglomeration of Fine Particles from Coal Combustion
The removal of fine particles in coal-fired fumes was experimentally studied based on acoustic agglomeration. An experiment facility was designed and set up. In this facility, a fluidized bed coal combustor was used as fume generator, and an Electrical Low Pressure Impact or (ELPI) was used to measure the fine particle concentration and size distribution in the fumes. The results show that under the effect of high intensity sound waves, there is good performance to remove fine particles in coal-fired fumes, which with a number mean diameter of 0.07μm. Especially, under the conditions of the frequency of 1 000Hz and the sound intensity of 161.5dB, the number concentration of 0.0233~9.314μm particles decreased by 85.2%, and their mass concentration decreased by 92.5%.