Emitter Surface Temperature Measurements of a 25-A Class Hollow CathodeThe axial emitter surface temperature profile is experimentally characterized for a 25-A class hollow cathode operating across a range of operating conditions. Profiles were measured using aratio pyrometry diagnostic featuring a fiber optic inserted into the emitter region using a fast motion stage. Emitter temperature is found to increase with increasing discharge current, decreasing flow rate, and increasing magnetic field strength. Across a range of 10 –29 A, the maximum emitter temperature increased 176 ºC, an order of magnitude more than the changes measured for flow rate or magnetic fields strength. Profiles were generally self-similar across all operating conditions, and the difference between maximum and minimum emitter temperature never surpassed 10%, indicating that this cathode design results in satisfactory emitter utilization across its operating envelope
Document ID
20220007948
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Scott J. Hall (HX5, LLC)
Timothy G. Gray (Glenn Research Center Cleveland, Ohio, United States)
Timothy R. Sarver-Verhey (Glenn Research Center Cleveland, Ohio, United States)
Hani Kamhawi (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 20, 2022
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: International Electric Propulsion Conference 2022
Location: Boston, MA
Country: US
Start Date: June 19, 2022
End Date: June 23, 2022
Sponsors: Electric Rocket Propulsion Society
Funding Number(s)
WBS: 729200.06.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
space propulsionelectric propulsionhollow cathodes