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Hermetic Seal reliability has been a major concern in the microwave industry for the past
35 years or more. While sealing problems have occurred with various materials and processes, none have approached the difficulties
encountered with sealing aluminum modules.
An informal survey conducted over the last seven years of companies soldering contemporary feedthroughs into aluminum modules revealed a
wide range of results when tested to meet military specifications. A few companies indicated no difficulties whatsoever, while the majority
of companies indicated a 15 to 40% failure rate of seals during in-house testing prior to shipment. Some companies reported higher failure
rates, with one as high as 98% in-process failures on a major program. While this was not a formally conducted study, it provided considerable
insight into the magnitude of hermetic sealing problems in aluminum housings.
Although these findings appear staggering on the surface, they are perfectly understandable when the typical contemporary feedthrough design
is analyzed for strain under required cyclic thermal environments. In fact, what is more difficult to understand is how any significant
yield could be obtained at all using contemporary designs. The root cause of the problem lies in the fact that seal designs being marketed
to the microwave industry generally predate the advent of aluminum as a primary hermetic packaging material.
Over the years, the focus on this problem has been one of process improvement, plating changes, and solder improvements. While these
activities produced some improvement in yields, the basic problem remained, and companies became accustomed to poor yields as a way of life.
As frequently happens, contact between companies provided comfort mainly in the fact that most were encountering similar problems, and
apparently, no one had the answer.
Some changes which were introduced and used by many companies with marginal results included replacement of gold plating with nickel,
tin or silver plating to avoid gold embrittlement; multiple pretinning and wicking of gold parts to remove gold prior to final soldering;
and use of Indium solders to introduce more flexibility in the solder joint. Analysis and extensive experience have shown that contemporary
feedthrough designs have a significant reliability problem, even with the elimination of gold embrittlement and the use of more flexible
solders.
These problems are attributed to the fact that contemporary designs do not provide for strain control of the solder joint within acceptable
limits. Without this specific control, the solder will be subjected to excessive strain during thermal cycling and will break down with
relatively few cycles. The change introductions reflected previously present additional problems and/or limitations. None of the alternate
platings solder as reliably and consistently as gold, therefore leading to more rework.
Nickel poses a particularly difficult problem in achieving consistent solder results even with stringent impurity and shelf life controls.
The tin plate limits solder temperatures, thereby, limiting choices of solder temperature for subsequent solder operations. While pretinning
and wicking of gold reduced or eliminated the embrittlement problem, it also precludes the achievement of consistent hermeticity results and
is costly. In many cases, pretinning alters the precision dimensioning of parts sufficiently to preclude their subsequent assembly. Finally,
use of indium solders can be expensive and limits the temperature of subsequent processes.
HERMETIC SEAL COST
The true cost of hermetic seals must include the cost of dealing with in-process failures in addition to the initial cost. A more appropriate
title for this article might be "The Cost of Hermetically Sealing Aluminum Housings". It is a difficult and frequently endless task to assess
overall cost associated with a design flaw. The intent of this article is to provide some guidelines to the relative cost of various methods
of providing hermetic feedthrough seals in aluminum packages. More specific costs can be obtained by substituting actual costs from company
histories in any of the areas given typical or average treatment herein.
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THE COST MODEL
The table at the right is a Cost Model which accommodates each of the sealing methods considered.
It is important in dealing with the model to reduce costs to averages. Any attempt to include
all costs in terms of actuals might become very cumbersome. Sensitivity testing will allow
determination of those factors which most affect the final outcome or decision process.
These driving factors may then be evaluated or reconsidered more closely to provide a more
refined analysis without wasting effort on non-drivers. Cost-incurring elements include
thermal cycling, leak testing, rework, re-inspection, material review board (MRB), electrical
retests resulting from failures, and scrap.
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SEAL COST MODEL*
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MODEL COST ELEMENT (1)
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STANDARD COSTS
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FAILURE
RELATED
COSTS
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Feedthrough
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X
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X
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Solder
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X
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X
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Assembly
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X
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Thermal Cycling
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X
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X
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Leak Tests
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X
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X
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Rework (include.Insp)
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X
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Electrical (Re-Test)
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X
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MRB
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X
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Scrap
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X
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TOTAL
SEAL COST = TOTAL STD COST + TOTAL FAILURE - RELATED COSTS
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Note (1) All costs should include
appropriate overheads.
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Thermal Cycling is not an insignificant cost. Extensive testing driven by high failure rates
may cause demand to dictate further capital investment. Eliminating testing can reduce capacity requirements and possibly
allow company growth without further capital investment. It is important to note that high yields through optimum seal
design can potentially eliminate some current standard testing as well as added failure related testing. Typically, current
stress testing programs are based on historically high failure rates and are used to accelerate failures to the early process
stages. Leak testing cost can be reduced in the same way as thermal cycling. Proper design can eliminate extra testing as
well as current basic testing. Rework obviously can represent a sizable cost, particularly if it occurs in the latter stages
of the process. Rework increases significantly after lidding, but can also be extensive on modules already populated with
components. Re-inspections are required after any rework to assure that cleanliness and reliability have not been compromised.
The further along the assembly is in process, the more costly this inspection may become. Electrical Retest may be required
after rework to ensure that functionality of the module has not been affected, before standard testing is resumed. MRB action
may be necessary if failures occur at final acceptance. The added administrative cost of conducting this action may be significant
depending on lot size in which the failure occurs and frequency of lot failures. Scrap can be very costly should failures be
non-repairable. Looking at some failure cost relationships, based on assumed or typical cost factors will shed some light on
the true cost of hermetic sealing and allow knowledgeable choices to be made regarding the design approach.
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The sample case shown (dotted line) indicates a four percent failure rate of feedthroughs and reflects a module with five feedthroughs
(that is, nominal complexity). The module repair cost is $150.00, resulting in an amortized added module cost of $30 or an added cost
per feedthrough of $6.
The four percent failure rate example is not uncharacteristically low for contemporary seals. As discussed previously, the average
survey failure rates reported were considerably higher. It is clear from the nomogram that the only factor that can reduce hermetic
feedthrough sealing costs significantly is the failure rate given the fact that a fixed number of feedthroughs are required and
improvements cannot be made in reducing failure-related module rework costs. It should be emphasized, the cost of repair presented
in the nomogram must reflect the total added failure-related cost as presented by the model.
Table 2 lists the most common Hermetic Seal design options available currently for aluminum housings. Designs A, B and C
are contemporary designs of straight-barrel or headed feedthroughs. The total cost range of these designs is significantly higher
than that of the other three options. This discrepancy is due to the vast rework requirements resulting from solder joint failures.
The cost of repair used here was a reasonably conservative $6 to $8 per feedthrough, which is based on a relatively low solder
failure rate of four percent. As indicated previously, typical reported rates have been much higher.
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ASSESSMENT OF VARIOUS SEAL DESIGNS IN ALUMINUM HOUSINGS (Table 2)
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Option
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A
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B
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C
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D
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E
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F
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Seal Design
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Contemporary Glass Seal / Sn/Pb Solder
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Ceramic / Sn/Pb Solder
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Ceramic- / reinforced glass seals with Sn/Pb solders
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Laser-weldable glass or ceramic
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Contemporary glass with gold- based solders Au/Sn, Au/Ge, Au/Si
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Aluminum (1) compatible glass to metal with Sn/Pb solders
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Effectively Addresses Primary Failure Mode (solder)
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No
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No
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No
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Yes
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Yes
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Yes
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Inherent Residual Stress at Room Temperature
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Low, <500 psi C
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Low, <500 psi C
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Low, <500 psi C
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Variable, dependent on construction
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High, 27,000 to 40,000 psi C>
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Low, <500 psi C
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Maximum Cyclic Stress (2)
DStress
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Moderately Low = Solder Yield Stress T&C
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Moderately Low = Solder Yield Stress T&C
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Moderately Low = Solder Yield Stress T&C
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High, >30,000 T&C
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High 30,000 psi C
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Moderately Low = Solder Yield Stress T&C
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Maximum solder strain (%)
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>35
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>35
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>35
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n/a
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Neg.
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Typ. <5%
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Application limited
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Subject to high solder failure rate - all applications
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Subject to high solder failure rate - all applications
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Subject to high solder failure rate - all applications
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Geometry critical - can be high risk w/o thorough analysis and/or empirical testing
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Geometry critical - can be high risk w/o thorough analysis and/or empirical testing
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Least restrictive on design geometry
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Feedthrough Cost Range (3)
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$1.00 to $2.00
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$8.00 to $12.00
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$1.50 to $3.00
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$7.00 to $11.00
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$1.50 to $3.50
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$1.50 to $2.50
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Total Seal Cost Range w/Min.Typ Rework (4)
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$7.00 to $10.00
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$14.00 to $20.00
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$7.50 to $11.00
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$7.00 to $11.00
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$1.50 to $2.50
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$1.50 to $2.50>
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Design Risk Factor
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Low
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Low
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Low
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Moderate to High
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High
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Low
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Process Risk Factor
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High
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High
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High
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Moderate
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High
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Low
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NOTES:
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(1) Covered by U.S.Patent# 4841101.
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(2) Over Std. MIL.Temp. Range of -65 to +125 Deg. C.
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(3) Includes any solder cost where applicable.
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(4) 4% rework used, except Aluminum Compatible Zero.
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C = Compression
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T&C = Tensile and Compression
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The laser-weldable feedthrough (option D), reflects a slightly lower total cost, which results entirely from its basic procurement cost.
It has been assumed for the purpose of this article that a typical failure rate for this design is zero when, in fact, some failure rate
could be expected due to the high cyclic stress levels encountered with this design.
Option E reflects a variant of option A whereby gold-based solders are used in lieu of soft solders. This design allows the use of
contemporary feedthrough seals that are slightly lower in cost, but the lower price is offset by the unusually high cost of gold-based
solder preforms, which produce an installed material cost approximately the same as option F the aluminum-compatible feedthrough.
Two potentially costly problems exist with the use of option E. The first possible problem is the added thermal stress on the aluminum
plating. Plating on aluminum, when properly applied, stands up well at temperatures of 250° to 275°C and allows for timely flow of
product from the plater. The gold-based solders (Au/Sn, Au/Ge and Au/Si) require a minimum process temperature of 310°C and up to 400°C.
Processing plated aluminum at these temperatures carries a significant risk of blistering. The cost impact of such failures is extremely
high in that rework likely incurs the loss of the feedthrough seals, as well as, the cost of stripping, replating and reassembling the
parts. If the housings have been post-machined for lid laser weldability, or plated with a masking process, the cost of plating rework
is increased greatly.
The second risk factor is the design risk with new geometries when using gold based solders. These solders are quite strong and actually
approach the strength of a braze. The fact that the seal glass is placed in high compression is good unless a geometric situation is
encountered. In this case, the aluminum yields locally adjacent to the seal, and causes the seal to crack. A number of commonly desired
configurations preclude the reliable use of gold solders.
When the aluminum yields locally adjacent to the seal, a total loss of the module results in the form of cracked seals with severe cost
effects. The only recovery from this problem is a fallback to the use of soft solder aluminum-compatible feedthroughs, which may require
housing changes and/or special feedthroughs to rectify, with the associated cost and schedule impacts. Many cases have been observed
where a fallback design was not considered and modules could not be delivered to the required specification, resulting in untold cost
and program delays.
Option F reflects the aluminum-compatible design, which utilizes a particular geometry and soft solders to provide a conformal solder
joint which reliably absorbs all of the thermally created strain, allowing significant numbers of thermal cycles without loss of
hermeticity.
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Two ranges of radial clearance are shown, representing contemporary seal designs and the aluminum-compatible design. Comparing the
radial gap (solder thickness) of the two designs reflects the significant difference in the degree of strain (elongation) to which
the solder joint is subjected. While this strain does not occur instantaneously with temperature change, it does occur essentially,
in total, after hours of dwell at temperature extremes.
The aluminum-compatible design reduces radial solder strain by approximately an order of magnitude over contemporary soft soldered
feedthrough seals. Zero failure rates are achievable, which results in a unit cost of a seal that is equal to that of its initial
acquisition and assembly cost. The elimination of seal failures can then lead to reduction and/or elimination of current in-process
testing when product confidence is gained.
Jack Pollock received his BSME degree from the University of New Hampshire. He was with Sanders Associates for 26 years
as a development engineer and program manager, leading such programs as the AN/ALQ-137 and AN/ALQ-137-4 countermeasures systems
for the FB-111 and EF-111 aircraft respectively, as well as the AN/USM-464 computerized flight line test set. Pollock founded
Product Engineering Associates, Inc. a consulting firm, and Special Hermetic Products Inc. in 1986 and 1990 respectively.
He is a registered professional engineer in New Hampshire.
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