Preliminary tests of annular ion opticsThe analyses and fabrication techniques used to develop a prototype 50-cm annular ion engine optics are described. Based on a finite element analysis of several different electrode geometries, the prototype ion optics was fabricated in the shape of a half torus dished into the annular discharge chamber. Results of thermal/mechanical characterization during extensive thermal cycle testing of the prototype ion optics are presented, together with results of initial beam extraction tests performed using Xe propellant.
Document ID
19920066152
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Aston, Graeme (NASA Lewis Research Center Cleveland, OH, United States)
Aston, Martha B. (NASA Lewis Research Center Cleveland, OH, United States)
Kolts, James B. (Electric Propulsion Laboratory, Inc. Tehachapi, CA, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 92-3148Report Number: AIAA PAPER 92-3148