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Development and testing of a 20 kHz component test bedA history of the General Dynamics Space Systems Division 20-kHz breadboard is presented, including its current configuration and its role in the SSF program. Highlights and results are presented of a series of tests conducted on the 20 kHz breadboard. The first test presented is the 20 kHz Breadboard Acceptance test. This test verified the operation of the delivered Breadboard and also characterized the main components of the system. Next, an in-depth efficiency testing effort is presented. The tests attempted to apportion all the power losses in the 20 Hz Breadboard Main Inverter Units. Distortion test data are presented, showing the distortion characteristics of a Mapham inverter. Lastly, current work on the 20 kHz Breadboard is presented including Main Inverter Unit paralleling tests. Conclusions are summarized and references given.
Document ID
19900051071
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Button, Robert M.
(NASA Lewis Research Center Cleveland, OH, United States)
Brush, Andrew S.
(NASA Lewis Research Center Cleveland; Sverdrup Technology, Inc., Middleburg Heights, OH, United States)
Sundberg, Richard C.
(General Dynamics Corp. Space Systems Div., San Diego, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Ground Support Systems And Facilities (Space)
Meeting Information
Meeting: IECEC-89
Location: Washington, DC
Country: United States
Start Date: August 6, 1989
End Date: August 11, 1989
Accession Number
90A38126
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Other

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