DocumentCode :
3346508
Title :
Thermal cycle reliability and failure mechanisms of CCGA and PBGA assemblies with and without corner staking
Author :
Ghaffarian, Reza
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2005
fDate :
31 May-3 June 2005
Firstpage :
391
Abstract :
Area array packages (AAPs) with 1.27 mm pitch have been the packages of choice for commercial applications; they are now starting to be implemented for use in military and aerospace applications. Thermal cycling characteristics of plastic ball grid array (PBGA) and chip scale package (CSP) assemblies, because of their wide usage for commercial applications, have been extensively reported on in literature. Thermal cycling represents the on-off environmental condition for most electronic products and therefore is a key factor that defines reliability. However, very limited data is available for thermal cycling behavior of ceramic packages commonly used for the aerospace applications. For high reliability applications, numerous area array packages are available with the same design pattern both in ceramic and plastic packages. This paper compares assembly reliability of ceramic and plastic package with the same I/O and pattern. The ceramic package was in the form of CCGA with 560 I/Os peripheral array with the same pad design as its plastic counterpart. The effects of the following key parameters on reliability of both CCGA and PBGA assemblies were investigated. Thermal cycle ranges, -50/75°C, -55/100°C, and -55/125°C; corner staking on failure mechanisms for two thermal cycle profiles, -55/125°C and -50/75°C; and package interchangeability, i.e. using PBGA package on CGA pad design with a larger pad; heat sink attachment on the top of package. Packages were assembled on polyimide board and their daisy chains were continuously monitored. Optical photomicrographs were taken at various thermal cycle intervals to document damage progress and behavior. Representative samples along with their cross-sectional photomicrographs at higher magnification, taken by scanning electron microscopy (SEM), are also presented. These were used to determine crack propagation and failure analyses for packages with and without corner staking.
Keywords :
assembling; ball grid arrays; ceramic packaging; chip scale packaging; crack detection; failure analysis; multichip modules; plastic packaging; reliability; scanning electron microscopy; -50 C; -55 C; 1.27 mm; 100 C; 125 C; 75 C; AAP; CCGA assembly; I-O peripheral array; PBGA assembly; SEM; aerospace application; area array packages; assembly reliability; ceramic package; chip scale package; column grid array; corner staking; crack propagation; cross-sectional photomicrograph; daisy chain; electronic product; failure analysis; failure mechanism; optical photomicrographs; package interchangeability; pad design; plastic ball grid array; plastic package; polyimide board; scanning electron microscopy; solder joint; thermal cycle reliability; thermal cycling; Assembly; Ceramics; Chip scale packaging; Electronic packaging thermal management; Electronics packaging; Failure analysis; Heat sinks; Plastic packaging; Scanning electron microscopy; Thermal factors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic Components and Technology Conference, 2005. Proceedings. 55th
ISSN :
0569-5503
Print_ISBN :
0-7803-8907-7
Type :
conf
DOI :
10.1109/ECTC.2005.1441295
Filename :
1441295
Link To Document :
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