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PEM Research
Alexander TeverovskyParts, Packaging, and Assembly Technologies
Office, Code 562, GSFC/ QSS Group, Inc.
Outline
Temperature limitations in PEMsHASTAcoustic microscopyWire bond qualityHow to improve PEM guidelines
July 2004 2
July 2004 3
What limits testing T for PEMs?
Maximum junctiontemperatureMax. operational temperature Max storage temperature Glass transitiontemperature of MC
• There is no standardized technique to determine Tj max and Tst(?)
• Absolute maximum ratings?• Mfrs. warn that exceeding these T
may cause permanent damage• Ex1: Tjmax=165 oC, Tst=150 oC• Ex2: Tjmax=100 oC, Tst=100 oC• Does exceeding Tg cause failures?
A methodology to determine BI temperature and conditions is needed.Does exceeding Tg cause failures?
July 2004 4
Tg Measurements: TMA
TMA2940PEM
Quartz probe
Thermocouple
July 2004 5
Does low Tg indicate Poor Thermal Stability?
TGA for MC with different Tg TGA measurements of MCs with different Tg showed that materials with Tg ~135 and 115 oC had higher stability compared to MC with Tg.The most thermally stable polymers, silicone rubbers and Teflon, have extremely low Tg of -20 to -120 oC for the rubbers and -90 oC for Teflon.
90
92
94
96
98
100
300 400 500 600temperature, oC
wei
ght,
%
170 C138 C173 C174 C133 CTg~173 oC
Tg~135 oC
Tg is not an indicator of thermal stability of MC
DTGA at 1 oC/min N2
-0.08
-0.07
-0.06
-0.05
-0.04
-0.03
-0.02
-0.01
0
250 300 350 400
temperature, oC
mas
s lo
ss ra
te, %
/min
Tg=169
green 115
Tg=146
Tg=165
July 2004 6
Effect of Tg on Failure Modes and Mechanisms
When characteristics of MC affect reliability of PEMs, the Tg effect might be expected.This is important for analysis of acceleration factors and for prediction of long-term reliability based on high-temperature stress testing.
Most probable case:Ts > Tc > Tg; λq >> λexper
Tg most likely will not affect results of standard S&Q testing
July 2004 7
Tg Effect SummaryChanges in failure rates at T>Tg are possible and should be considered for analysis of acceleration factors and prediction of long-term reliability of PEMsbased on high-temperature stress testing.
Experimental data did not reveal the effect of Tg on results of standard screening and qualification testing.
For a normal quality lot there is no immediate danger in exceeding Tg during standard reliability testing.
TMA of plastic packages has been proven to be an important tool for FA and reliability evaluation of PEMs.
July 2004 8
HASTBiased HAST is the most sever environmental test (~ 30% to 50% chance of failure)Is HAST adequate to normal conditions?(130 oC > Top, swelling, delaminations, acceleration: 100 hr >100 years)Biased HAST win-win testing for space applications?Still… moisture can penetrate to die and cause failures.Moisture concentration depends mostly on RH, not on T. Temperature significantly accelerates penetration.Unbiased HAST might not reveal moisture-related failures.We do need an adequate accelerated testing to assess the effect of moisture for space applications.
July 2004 9
Opamp SMT simulation and HAST results
Part Type Pack DC SMT HAST Comm.
OP1 Instr. SOIC8 0030, 0110 1/30, 0/30
30/30, 27/30 Param. failures
OP2 Quad SOIC16 0101 16/30 2/30 SMT: IOS and AOL HAST: init.+1 new
OP3 Instr. SOIC8 0022, 9628 0/16, 0/16 0/16, 0/16
OP4 Bandw SOIC8 0018 0/30 0/30
OP5 Bandw SOIC8 0041 0/30 0/30
OP6 Dual SOIC8 0033, 0109, 9946
0/30, 0/30, 0/30
0/30, 0/30, 1/30
Possibly reverse installation
OP7 Precis. SOIC8 0019, 0021, 0029
0/30, 0/30, 0/30
0/30, 0/30, 0/30
OP8 Quad SOIC16 9945 2/30 0/28
July 2004 10
Distribution of Biased HAST FailuresFailures during biased HAST
0
20
40
60
80
100
0 200 400 600 800 1000
time, hr
failu
res,
%
130 C
150 C
110 C
Arrhenius plot of median life
10
100
1000
2.3 2.35 2.4 2.45 2.5 2.55 2.6 2.65
1000/T, 1/K
med
ian
time,
hr
Ea = 0.59 eV
Ea is lower than in Peck-Hallberg model: 0.79 -1.1 eV.This increases the probability of failures at low T.
July 2004 11
Arrhenius-Weibull model
10.00
1.00E+5
100.00
1000.00
10000.00
450.00300.00 330.00 360.00 390.00 420.00
Life time prediction at 85% RH
temperature, K
time,
hr
2.2 years Ea = 0.59 eV
HAST at 85% RHT = 110, 130, and 150 deg.C
1% failures
July 2004 12
RT Testing after Unbiased HASTRT bias testing after
110 oC HAST for 800 hrs
0.3
0.35
0.4
0.45
0.5
0.55
0 500 1000 1500
time, hr
IPS,
mA
Failures during RT testing followed unbiased HAST
0
20
40
60
80
100
0 200 400 600
time, hr
failu
res,
%
after 150C/85%/130hr after 130C/85%/350hr after 110C/85%/800hr
RT testing followed unbiased HAST resulted in failures in 24 to 600 hours.PEMs retain moisture for some time after HAST.
July 2004 13
Moisture diffusion and retention in PEMs
Note: C - moisture concentration on the die surface;M - mass of moisture in the package;C/Co = 1 corresponds to moisture saturation at 100% RH.
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
0.01 0.1 1 10 100
time, hr
C/C
o, M
/Mo C/Co soaking
M/Mo soakingC/Co testingM/Mo testing
Example:Package 2mm
Soak conditions: 110oC/85%/48hr, unbiased.
Test conditions: 85 oC, bias.
Soaking
Testing
July 2004 14
HAST Summary
Biased HAST is a too severe test for space applications.Unbiased HAST is far less severe and might not reveal failures. However, post-HAST testing at RT under bias causes failures.A combination of unbiased HAST with LT bias testing might be a good alternative to biased HAST for QA of parts intended for space applications.
July 2004 15
C-SAM: SWIFT StatisticsRejectable delaminations were observed in 4 out of 6 types of power devices and in 14 out of 23 types of linear devices.
The proportion of rejects varied from 2.3% to 28% for power devices and from 0.14% to 83% for low-power devices.
The cost of AM is relatively high, up to $8 per part, even for alarge quantity lot.
Out of 31,090 parts subjected to screening, 565 (1.8%) were rejected by electrical testing and 3,586 (11.5%) by CSAM.
Acoustic microscopy rejected far more parts than did electrical measurements. Are all these rejects potential failures, and if so, what is theconfidence in quality of a lot with ~10% rejects?
July 2004 16
CSAM: Which Part to Choose?Delaminations are due to stress relief in PEMs.
This part might operate reliably because
mechanical stresses have been relieved and
delaminations are stable.
This part might fail if the stresses have not been
relieved and delaminationsdevelop in critical wire bond
areas.
Typically rejected Typically accepted
CSAM is a nondestructive test, but can damage the parts.If delaminations are serious defects, is it possible to improve reliability of a lot with 5% to 50% rejects by screening?Is CSAM useful for screening?
Before stress. After stress?Before stress. After stress?
July 2004 17
Changes in Delaminations Due to Stress Testing (Power Devices)
Die surface Leads
Top paddle
0
20
40
60
init after SMT after 1000TC
after HT TC
dela
min
atio
ns, %
FET2FET1FET3
0
20
40
60
80
100
init after SMT after 1000TC
after HT TC
dela
min
atio
ns, %
0
20
40
60
80
100
init after SMT after 1000TC
after HTTC
dela
min
atio
ns, %
FET2FET1FET3
The proportion of delaminations can vary significantly after solder reflow and environmental stress testing
July 2004 18
Results of Temperature Cycling of Parts with Excessive Delaminations
Part SMT TC0 100 TC0 3000/30 0/30
0/300/300/300/300/300/300/300/30
0/300/300/300/300/300/300/300/30
TC0 1k TC1 300 TC2 300PEM1 0/30 0/30 0/15 0/15PEM2 0/30 0/30 1/15 1/15PEM3 0/30 0/30 0/15 0/15PEM4 0/30 0/30 0/15 0/15PEM5 0/30 0/30 0/15 0/15FET1 0/30 0/30 0/15 0/15FET2 0/30 0/30 0/15 0/15FET3 0/30 0/30 0/15 0/15
PEM6* 0/30 0/30 - -
*Parts had excessive delaminations at finger-tips after HAST.
July 2004 19
CSAM SummaryParts with excessive delaminations at the paddle and leads (at secondary bond locations) had no electrical failures after 1000 TC at –55 to +125 oC conditions.
The analyzed power devices in TO220-style packages are prone to formation of top-of-die delaminations; however, no wire bond fractures occurred even after multiple temperature cycling.
No correlation between the proportion of delaminations and flux-induced leakage currents were observed indicating a failure of CSAM examination to screen out potential failures.
For the part types used, CSAM examination likely is not a value-added technique for screening; however, it is very useful for qualification testing.
July 2004 20
Wire Bonding: problems recognized by manufacturers
Lifted bonds in various SOIC-type (14/16/20/24 pins) widebody package
parts assembled by NSEM between Feb and Nov 2002
R.Sampan, R Kuang(Actel), CMSE’03:Hermetic gold bonded devices with contamination on bond pads may pass bond pull test at as-bonded condition but fail after 80 hrs at 150°C.
Degradation and failures in poor quality wire bonds might happen with time even at relatively benign storage
conditions.
July 2004 21
Wire Bonding: examples of previously previously revealed problems
Failures in parts manufactured in 1999 were observed during board-level testing in 2002 (FA: contamination-induced WB degradation).
COTS FPGA failed DPA due to poor wire bonding (2003).
A detector failed in 2002, three years after manufacturing due to degraded WB (Al wire to Au post).
A lifted wire in an ASIC packaged in
PQFP was revealed during failure analysis
(2003).
July 2004 22
Wire Bonding: problems 2004SDO:MTK-WCG-DF-0412 ASIC ceramic packageLifting at 1.9 g.
VMI hybrid plastic XA-16 ASIC ceramic
STEREO
GLAST: photodiodes+all ASICsin plasticQFP
Substantial portion of reliability issues are now at the packaging level.Development of a non-destructive technique for WB qualification in PEMs is important.
July 2004 23
Examples of WB degradation after HTSLMost WB were lifted showing porous structure of intermetallics. The peripheral area of Al around the bonds had multiple voids. The appearance of voids suggested diffusion of Al atoms towards the WB along the crystalline grain boundaries. For LT the appearance of the voids suggested a corrosion attack (possibly H3C-Br).
July 2004 24
Technique for Evaluation of WB Quality
Rc measurements:VF of P-N junctions used in the input/output ESD protection circuits are measured before and after the stress
MeasureVF0
StressMeasure
VF1
δRc = (VF1 – VF0)/IF
This technique is simple, does not require full electricalcharacterization, and have an accuracy ~ 0.3 Ohm.
July 2004 25
Example of early WB failuresWeibull-Arrhenius plot
THS
1% failures after ~ 1 year at 100 oCFA results: failures were due
to WB degradation
Wire bond degradation might cause failures even at relatively low temperatures of ageing
July 2004 26
WB Infant Mortality Failures
100.00 10000.001000.000.10
0.50
1.00
5.00
10.00
50.00
90.00
99.00
0.10
time, hr
cum
ulat
ive
prob
abilit
y, %
infant mortality failure
HTSL at 190 deg.C99% confidence bounds
This part had also WB
failures after HAST
July 2004 27
Degradation of contact resistance
0
20
40
60
80
100
0.1 1 10 100Rc, Ohm
accu
mul
ated
per
cent
120 hr
210
346
530
690
970
Distributions of Rc in air
0.1
1
10
100
0 500 1000 1500 2000
time, hr
med
ian
Rc,
Ohm
OP vacOP airLT vacLT air
air
vacuum
Kinetics of Rc variations
WB degradation in vacuum is much lesser than in air.After ~1000 hrs in air ~70% of WBs had Rc >10 Ohm; in vacuum Rc < 3 Ohm even after 1500 hrs.
July 2004 28
WB problems: SummaryWB degradation limits HT reliability of PEMs
WB is a real problem; however, it is not addressed in the guidelines.
Forward voltage drop measurement technique might be useful for WB qualification, life prediction and revealing IM failures.
There is a critical temperature, after which the rate of WB failures changes.
Vacuum testing might provide high acceleration without introducing new failure modes.
July 2004 29
Evolution of Parts Engineering for PEMs
Rule-based(MIL parts)
Knowledge-based(COTS PEMs)Phase I, II, ..
No wear-out, no damaging testing.
Reliability is mostly limited by defects => the importance of infant mortality and screening.
Element and package size reduction easier to damage.
Reliability is limited by intrinsic wear-out mechanisms => qualification is more important than screening.
Government maintains the standards and is responsible for reliability provided all criteria are satisfied.
PEs are responsible for reliability evaluation and mitigation of risks associated with use of COTS PEMs.
July 2004 30
Catch-22 in ScreeningLiterature data and our experience:Screening might not add value and might negatively impact reliability of high-quality components.However, for low-quality components, screening should be maintained.
Do not screen lotswith low IM
Screen the lot to reveal
IM
testi
ng
testi
ng
To break this circle, make BI and CSAM optional, depending on results of extended qualification.Perform qualification on unscreened samples with interim measurements and let the parametric/functional failures to go through. This will identify possible failure modes, evaluate the risk of failures, show whether the screening is necessary, and reduceoverall S&Q costs.
July 2004 31
A Feedback System to Improve S&Q
Most project test data are wasted; obtaining statistics of failures is not easy. (Projects are often not concerned about failures <PDA)Test results might be deceptive. (Rejects might be due to poor electrical measurements and/or damage during testing.) FA results might be insufficient. (FA might be performed only tomitigate the risk for the mission.)Do not miss an interesting failure case (WB infant mortality)
Projects are generating a lot of data.Learn from our experience.
QASAccumulation and analysis
of project data LL
Analysis of literature data
Additional evaluation and testing
July 2004 32
Revision of PEM GuidelinesMake CSAM optional provided extensive qualification using acoustic microscopy is planned. Allow qualification of non-screened devices provided a larger quantity of parts with interim measurements, failures going through, and analysis of failed parts, is performed.The proportion of area where intermetallics at Au/Al wire bond are formed should be evaluated during DPA. If < 50 %, additional evaluations is necessary (WB package-level qualification).Remove Tg limitations for BI.Eliminate flux application during preconditioning.Replace HAST with a combination of HAST and biased testing at RT.
July 2004 33
Some Trends for Improvement of the Guidelines to Discuss in Future
Put more emphasis on evaluation rather than on DPA. Addressing concerns rather than rejecting suspicious parts.
More attention to qualification rather than to screening.
Replace existing 3-level S&Q test flows with specially designed application-dependent plans.Use alternate techniques for S&Q:
noise measurements;Non-linearityRc measurements for WB qualification.Thermal impedance for power devices.…