| Created: 5/21/95 |
Updated: 4/18/97 |
Finite Element Modeling of Advanced Interconnections
Objectives
Develop detailed Finite Element Analysis (FEA)
models that allow computation of thermal,
thermomechanical, and mechanical responses
for Advanced Interconnect Technology (AIT)
packages. Develop these models into software
tools.
Background
AIT packages are multichip modules (MCMs)
that utilize advanced packaging technology for
interconnections between chips. For new
technologies, it is important to understand
potential reliability problems and failure
mechanisms in order to develop suitable
technology characterization and qualification
procedures.
This modeling effort forms part of a joint
NASA-Army-Navy-Air Force Reliability
Technology (RELTECH) program to develop a
detailed understanding of reliability of AIT
structures in space and military environments.
New packaging technologies, will be analyzed
such as GE's overlaid high-density
interconnects (HDI), which places active chips
within wells formed on the substrate and then
overlays dielectric layers, containing current
traces for interconnection. Chip's multichip
modules and other technologies, such as three-
dimensional die stacks, are also being examined
as part of the program.
Approach
The effort consists of developing global and
local three-dimensional FEA models for
analyzing AIT structures. The global models
provide analysis at the package level, while the
local models provide refined analyses of
specific vulnerable substructures. During the
global modelling procedure, dimensions for
such structures as the substrate, the wells within
the substrate, and the chips are established. The
material property for the overlaid
interconnection layers is described using a rule
of mixtures.
On the local model level, geometry for
structures such as vias, bond pads, metallization
lines and various material interfaces are
established, and the exact material properties
are used. The finite element models are
automatically generated and analyzed for user-
input dimensions and material properties. Each
model is integrated into a generic software tool
for government, customer, and CALCE EPRC
use, with flexibility to extend capabilities to
include newly developed AIT technologies.
The software tool facilitates model building and
interpretation of results. The models analyze
the AIT module's global and substructural
responses to thermal, thermomechanical, and
mechanical loads caused by external thermal
cycling, mechanical loads, and device power-on,
power-off. The AIT tool can be used to
examine potential failure mechanisms and to
assess the limits of operating conditions and
external environments that cause failures.
Work Accomplished
- Global and local finite element models have
been developed for the GE-HDI technology,
and preliminary thermomechanical finite
element analysis has been performed for an
HDI test structure.
- Software tools have been developed for
automating model building, material
database entry, and display of results.
- Models are being developed for n-Chip's
MCM and three-dimensional die-stacks.
- The Jet Propulsion Laboratory (JPL) is
interfacing the AIT module with the
NASTRAN finite element analysis codes.
- PDA engineering (the developer of Patran)
is developing the AIT software into a
submodule for Patran.