Microcircuit manufacturers of Plastic Encapsulated Microcircuits (PEM’s) have made changes in epoxy molding compound materials and chemistry, which lower Glass Transition Temperature (Tg). PEM users in harsh environments have concerns if either the part in its application, or in evaluation or assembly, is used close to, or above, the Tg. Various Tg measurement techniques are available and discussed. Test results from one technique is reviewed. The implications of the Tg results on usage of these parts in space applications will be presented. Burn-in/ reliability test results of samples with low Tg PEM’s will be presented. The reliability experiments include testing under different temperatures. The issue being addressed is whether outgassing of molding compounds occurs when the temperature of the molding compound exceeds the Tg. This is a caution noted by many vendors. As an example outgassing of flame retardants can degrade parametric performance and wire bond integrity. This would be the case when PEMS are being qualified for Space applications using burn-in or in storage environments. JPL’s past experience has shown that COTS PEMS parametrics can degrade significantly even when the burn-in temperature is well below the Tg. Two different microcircuits exhibiting low Tg were evaluated. Assessment of final electrical test measurements and yield are shown.
Skip Nav Destination
ASME 2003 International Electronic Packaging Technical Conference and Exhibition
July 6–11, 2003
Maui, Hawaii, USA
Conference Sponsors:
- Electronic and Photonic Packaging Division
ISBN:
0-7918-3690-8
PROCEEDINGS PAPER
Reliability of Low Glass Transition Temperature COTS PEM’s for Space Applications
M. Sandor,
M. Sandor
California Institute of Technology, Pasadena, CA
Search for other works by this author on:
S. Agarwal,
S. Agarwal
California Institute of Technology, Pasadena, CA
Search for other works by this author on:
D. Peters,
D. Peters
California Institute of Technology, Pasadena, CA
Search for other works by this author on:
M. S. Cooper
M. S. Cooper
California Institute of Technology, Pasadena, CA
Search for other works by this author on:
M. Sandor
California Institute of Technology, Pasadena, CA
S. Agarwal
California Institute of Technology, Pasadena, CA
D. Peters
California Institute of Technology, Pasadena, CA
M. S. Cooper
California Institute of Technology, Pasadena, CA
Paper No:
IPACK2003-35177, pp. 809-815; 7 pages
Published Online:
January 5, 2009
Citation
Sandor, M, Agarwal, S, Peters, D, & Cooper, MS. "Reliability of Low Glass Transition Temperature COTS PEM’s for Space Applications." Proceedings of the ASME 2003 International Electronic Packaging Technical Conference and Exhibition. 2003 International Electronic Packaging Technical Conference and Exhibition, Volume 1. Maui, Hawaii, USA. July 6–11, 2003. pp. 809-815. ASME. https://doi.org/10.1115/IPACK2003-35177
Download citation file:
7
Views
Related Proceedings Papers
Related Articles
Effects of High-Temperature Storage on the Glass Transition Temperature of Epoxy Molding Compound
J. Electron. Packag (March,2021)
Wire-Sweep Study Using an Industrial Semiconductor-Chip-Encapsulation Operation
J. Electron. Packag (December,1997)
Die Pad Anchoring Designs for Enhanced Adhesion Integrity in IC Packages
J. Electron. Packag (September,1993)
Related Chapters
Introductory Survey
Introduction to Plastics Engineering
Diamond Is a GAL's Best Friend
Hot Air Rises and Heat Sinks: Everything You Know about Cooling Electronics Is Wrong
Containments for Transportation and Storage of Spent Nuclear Fuel and High-Level Radioactive Material and Waste
Online Companion Guide to the ASME Boiler & Pressure Vessel Codes