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Structural evaluations and dynamic testing of solar electric propulsion components.Results of an experimental and analytical study of selected Solar Electric Propulsion (SEP) thrust subsystem components are presented. A mass and center-of-mass mockup of an experimental power conditioning (PC) panel was used for the PC structure evaluation. Test environment was based on that specified for prooftesting the Viking spacecraft electronics. Modal frequencies were surveyed over the range of 0-2000 Hz using both conventional test equipment and the holographic interferometry technique. Results of the forced vibration tests point to the need for some additional stiffening to make the structure qualifiable.
Document ID
19720045275
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Womack, J. R.
Chen, J.-C.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Subject Category
Auxiliary Systems
Report/Patent Number
AIAA PAPER 72-442
Report Number: AIAA PAPER 72-442
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Electric Propulsion Conference
Location: Bethesda, MD
Start Date: April 17, 1972
End Date: April 19, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A28941
Distribution Limits
Public
Copyright
Other

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