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Arc discharge supply component protection circuitryIn a mercury-bombardment ion engine, the discharge supply is a high-current low-voltage one that maintains an arc or discharge inside the engine. In a 30-cm engine the supply provides up to 45 volts at about 13 amperes and is referenced at approximately 1100 volts above ground. Due to the engine discharge characteristics, a very slow feedback control loop is required. A high-speed current limit must be used to protect the components in the power conditioner, a pulse-width-modulated bridge inverter. A high-speed cycle-by-cycle current-limit circuit which allows the inverter to continue running in an overcurrent condition is used to protect it. The high-speed current sensing allows the inverter to be turned off each half cycle before the current in the primary of the inverter exceeds a safe level. This permits the inverter to continue to provide current into a discharge or a fault condition, until the feedback control system can actively control the current.
Document ID
19770058119
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Ahrens, A. F.
(Hughes Aircraft Co. El Segundo, CA, United States)
Cardwell, G. I.
(Hughes Aircraft Co., Space and Communications Group, El Segundo Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1976
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Power Electronics Specialists Conference
Location: Cleveland, OH
Start Date: June 8, 1976
End Date: June 10, 1976
Accession Number
77A40971
Funding Number(s)
CONTRACT_GRANT: NAS3-17223
Distribution Limits
Public
Copyright
Other

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