• DocumentCode
    344686
  • Title

    A systems approach for quality and reliability of chip scale package assembly

  • Author

    Ghaffarian, Reza

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    2
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    289
  • Abstract
    This paper reviews many factors that affect interconnect reliability of commercial-off-the-shelf (COTS) chip scale package (CSP) assemblies. These include: package type, package build, board design, and assembly variables. Methods of accelerated environmental testing were discussed and reasons for unrealistic life projections for CSP assembly reliability by numerous modelers is also examined. Preliminary thermal cycling test results in the range of -30°C to 100°C for test vehicles, especially a double sided assembly were also presented. It was concluded that availability of meaningful assembly reliability test results are needed to accelerate implementation of this technology. The JPL-led CSP consortia are addressing many of these issues
  • Keywords
    ball grid arrays; chip scale packaging; concurrent engineering; environmental testing; integrated circuit interconnections; integrated circuit reliability; life testing; microassembling; -30 to 100 C; BGA; COTS chip scale package assembly; accelerated environmental testing; assembly quality; assembly variables; board design; concurrent engineering; double sided assembly; interconnect reliability; package build; package type; solder joints; systems approach; thermal cycling test; underfill; unrealistic life projections; Assembly systems; Benchmark testing; Chip scale packaging; Electronic packaging thermal management; Electronics packaging; Laboratories; Life estimation; Life testing; NASA; Propulsion;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 1999. Proceedings. 1999 IEEE
  • Conference_Location
    Snowmass at Aspen, CO
  • Print_ISBN
    0-7803-5425-7
  • Type

    conf

  • DOI
    10.1109/AERO.1999.793173
  • Filename
    793173