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Reliability Evaluation of MIT/LL FDSOI 0.25 mm Process for Space Applications
File Name: SharmaTeverovskyReliabilityEvalArticle.pdf | Date Submitted: 10/02/01
 

File Size:
38KB
Document Author
Ashok Sharma - asharma@pop300.gsfc.nasa.gov
Goddard Space Flight Center
Phone: 301 286-6165 | FAX: 301 286-1695
[Additional User Information]

Download "Reliability Evaluation of MIT/LL FDSOI 0.25 mm Process for Space Applications" (38KB) Now.
 
Description:
EEE Links - July 2001 Article
 
Abstract:

The previous report entitled, "Reliability Evaluation of Fully Depleted SOI (FDSOI) Technology for Space Applications," posted on the NEPP web site, provided a general overview of SOI technology including materials, process, reliability issues, and MIT/LL FDSOI processes and associated reliability test structures. The hot carrier degradation effects in the MIL/LL FDSOI FETs at Vg = Vd/2 conditions, which are known to maximize the interface trap generation have been investigated at JPL [1].

This report (Part II) of the continuing evaluation, addresses characterization of the N- and P-channel transistors, including scaling effects and estimation of the reproducibility of the front- and back-channel parameters was performed. The transistor measurements included threshold voltage, subthreshold slope, mobility of charge carriers, gate leakage currents, and investigation of the edge effects. Radiation effects and charge instability in FD SOIFETs will be discussed in part III of the report.

 
Related Project(s):
EPAR (Electronic Parts)
 
Related Area(s) of Emphasis:
Advanced and Emerging Technologies

 
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