NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Deducing Electronic Unit Internal Response During a Vibration Test Using a Lumped Parameter Modeling ApproachNo abstract available
Document ID
20160005636
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
Authors
Van Dyke, Michael B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
May 2, 2016
Publication Date
March 25, 2014
Subject Category
Electronics And Electrical Engineering
Meeting Information
Meeting: Aerospace Testing Seminar
Location: Los Angeles, CA
Country: United States
Start Date: March 25, 2014
End Date: March 27, 2014
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available