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Thermal Cycling/Shock Behavior of CSP Assemblies
File Name: RezaGhaffarianArticle7101Links.pdf | Date Submitted: 10/02/01
 

File Size:
91KB
Document Author
Reza Ghaffarian - Reza.Ghaffarian@jpl.nasa.gov
Jet Propulsion Laboratory
Phone: 818 354-2059 | FAX: 818 393-5245
[Additional User Information]

Download "Thermal Cycling/Shock Behavior of CSP Assemblies" (91KB) Now.
 
Description:
EEE Links - July 2001 Article
 
Abstract:
A JPL-led chip scale package (CSP) Consortium of enterprises, composed of team members representing government agencies and private companies, recently joined together to pool in-kind resources for developing the quality and reliability of chip scale packages (CSPs) for a variety of projects. The experience of the Consortium in building more than 150 test vehicle assemblies, single- and double-sided multilayer PWBs, and the environmental test results has now been published as a chip scale package (CSP)guidelines document and distributed by Interconnection Technology Research Institute (ITRI).

The Consortium assembled fifteen different packages with I/Os from 48 to 784 and pitches from 0.5 to 1.27 mm on multilayer FR-4 printed wiring board (PWB). Another test vehicle was designed and assembled by a team member using their internal resources and was identified as TV-H. The TV-H assemblies were subjected to numerous thermal cycling conditions including -55°C to 125°C with two ramp rates, one thermal cycle with 2° to 5° C/min and the other near thermal shock. Cycles-to-failure (CTF) test results to 1,000 cycles and 400 cycles under these conditions are presented for 180 and 208 I/O fine pitch ball grid arrays (FPBGAs) with three die sizes. Decrease in CTFs due to ramp rate and die size increase for different I/O FPBGAs with 0.8 mm pitch are compared and analyzed.

 
Related Project(s):
EPAC (Electronic Packaging)
 
Related Area(s) of Emphasis:
High Density Packaging Technologies

 
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