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An optical technique to measure ion engine grid distortion due to differential thermal expansionThis paper describes an optical technique developed for measuring small differential grid displacements due to thermal expansion of an ion thruster accelerator system. The technique is based on confocal scanning optical microscope type II. For the measurements of small displacements where there are distances on the order of a meter or more between the lens plane and the sample, some of the optical components are moved while the sample is kept fixed. The feasibility of applying this technique to measure the thermally induced ion thruster grid displacements was demonstrated in a bench-top simulation. It is noted that this technique can also provide information on grid movement resulting from thermal transients such as the start-up.
Document ID
19900055558
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Trava-Airoldi, V. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Garner, C. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pivirotto, T. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Brophy, J. R.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 90-2650
Accession Number
90A42613
Distribution Limits
Public
Copyright
Other

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