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Eight-cm mercury ion thruster system technologyThe technology status of 8 cm diameter electron bombardment ion thrusters is presented. Much of the technology resulting from the 5 cm diameter thruster has been adapted and improved upon to increase the reliability, durability, and efficiency of the 8 cm thruster. Technology discussed includes: dependence of neutralizer tip erosion upon neutralizer flow rate; impregnated and rolled-foil insert cathode performance and life testing; neutralizer position studies; thruster ion beam profile measurements; high voltage pulse ignition; high utilization ion machined accelerator grids; deposition internal and external to the thruster; thruster vectoring systems; thruster cycling life testing and thruster system weights for typical mission applications.
Document ID
19740027087
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 74-1116
NASA-TM-X-71611
Report Number: AIAA PAPER 74-1116
Report Number: NASA-TM-X-71611
Meeting Information
Meeting: AIAA/SAE 10th Propulsion Conf.
Location: San Diego, CA
Country: United States
Start Date: October 21, 1974
End Date: October 23, 1974
Accession Number
74N35200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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