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15 september 2005 page 1/31
44th CEEES Meeting
Minutes of R and ESS WG
Meeting location : Hotel NOVOTEL Paris
Date : 24th October 2005
Attendees : see list hereafter
15 september 2005 page 2/31
Name
1st
name
Company/Society phone
fax email
RUDING Gunnar Ass. of Swedish Engineering
Industries /SEES
46 8 653 0418 46 8 653 0419 [email protected]
GRZESKOWIAK
Henri MBDA F /ASTE +33 1 34 88 35 23 +33 1 34 88 34 75
[email protected] office
[email protected] home
HOLY
Michel retired/SSEE +41 1 865 46 68 [email protected]
PALMEN Helge VTT Industrial Systems /SEEF +358 9 456 56 31 +358 9 456 7042
PEREGO Marco Angelantoni Industrie SPA +39 075 8955 213 +39 075 8955 200 [email protected]
WEETCH Colin e2v Technologies/SEE + 44 1245 453654 [email protected]
15 september 2005 page 3/31
1 - ADOPTION OF THE 43rd
CONGRESS R&ESS MEETING MINUTES
The minutes are adopted.
2 - Apologies FOR ABSENCES
No.
3 - INTRODUCTION OF NEW MEMBERS
No new member.
5- ESS ACTIVITY
It was agreed that there is a need for a basic terminology of terms relative to the tests , environmental
engineering and reliability such as MTBF, MTTR, reliability test, accelerated test ….
It was proposed that all the members send a list of these terms , with the known definitions and
corresponding source, to Marco , that will arrange a digest of all these inputs for next meeting.
Michel has proposed a list ( see in attachment 1). This list has been examined during the meeting.
Durability : HG will provide next time the definition (adopt the definition of the IEC56) ; as it is related
to the cost, is it affiliated to the life cycle cost ? Refer to the IEC 56.
Michel Holy wonders if there is a Mathematical relation between Reliability and Maintnability ?
Helge will examine the compatibility between the proposed terminology and IEC one.
HG will provide return from reliability and statistician collegues on mathematical description.
Michel Holy will provide quick definitions of abbreviations. He is requesting to verify that the structure
of the terms is complying with the content of the definition of the related terms.
6- R ACTIVITY
7-
6.1 Life cycles environmental profile
It has been also decided in London to work of the product life cycles .
Extract from London meeting report : “
• The expected life profile of a product in different sectors of activity *, which is an important
issue to consider in product sustainability growth
o Output : life cycle environmental profile characterisation : climatic related parameters
such as number of cycles, temperature range , rate of change , humidity, pressure if
relevant, chemical contaminents , etc.)
or mechanical related parameters such as PSD for vibration, SRS or time histories for
shock, etc.
• Operational use :
o Dormant periods ( storage)
o Functional activation( ON/OF, junction temperature elevation, electrolytic
phenomenon,etc.)
• Identify the expected processes or modes of failure
• Assess the life duration of different type of technologies
*The sectors of acitivity covered by the current members are : mobile phones, telecommunication,
automation/robotics, nuclear power plant, control of climatic chambers, electronics in automotive
industry, missiles.”
Henri is proposing as a beginning to consider the following documents in which there are elements on life
cycle profile description:
15 september 2005 page 4/31
- French CIN EG 1 “ Taking into account the Environment through a
product development ( see an English version as attached document)
- An example of life cycle description ( see a french version as attached
document )
- Hank Caruso fundamental paper on LCEP , presented at IEST ( distributed during the current
meeting) .
- Henri has evocated the Strength / Stress approach ; the general appendix of GAM EG 13 is
describing this approach in one appendix ( see annex 14 of General Appendix of GAM EG 13 in
French , attached to the meeting report , in French)
Henri has also introduced a document dedicated to program management structuration : EN 9200 .
The work will be continued on the example of life cycle description on the mobile equipment dedicated to
pollution measurement.
6.2 Different types of tests
6.2.1 List of withhold tests
Type of test In charge of
feasability , design aid Colin Done : see att.3
Development test Michel
Reliability growth test (RGT) Collin
Aggravated tests Henri Done : see att.4
Accelerated tests Helge
Qualification Aad *
Reliability demonstration Collin
ESS including HASS Bob for ESS
( Henri for
HASS)
Acceptance test Bengt *
Production reliability acceptance test (PRAT) Bob
Pre production (zero production) Gunnar
Life duration Collin
Verification (validation) Bengt *
* to be confirmed
6.2.2 Template to apply to each of these tests
1 Test objective (purpose,definition…)
2 What is driving you for performing the test ?
3 Level of assembly of the product submitted to test
4 Number of items submitted to test
5 Type of product relevant to be submitted to the test ( mass volume low price product ,..)
6 Test duration (days, weeks, months..)
7 Separate or combined environments
8 Product strength and environment stress variabilities are or aren’t considered
( in the process of deriving the test severity)
9 Does the test bring knowledge on reliability parameters ?
10 Does the test consume totally or partially the life potential ot the equipment submitted to test ?
11 main norms , standards, technical references relative to this type of tests
For next meeting : the proposed persons will try to apply the template to the corresponding test .
15 september 2005 page 5/31
Accelerated tests by Helge Palmen ( see attachment 4)
Accelerated stress (Objective : identify product weaknesses by stimulation ) and accelerated life testing
(simulation of the field stresses) : a long discussion has taken place in order to clarify the differences
between the 2 types of tests. Helge will try to fill the ablove template for the 2 tests in order to clarify the
differences. There are still unexpected statements as Helge considers that stimulation ( in the
accelerated stress approach) may be established using models. That is not normally the case ( see the §
on aggravated tests = highly accelerated tests in attachment 3).
ESS and highly accelerated tests ( such as HALT) are not affiliated to the family of “Accelerated tests”
because acceleration in this latter family is based on a failure model making the relation between an
excitation and the expected failure . That is not the case in the highly accelerated tests.
Henri G. has indicated that there are 2 type of accelerated tests :
The first one is based on a physical model on the failure ( such as 5th power law)
The second is based on statistical description of the failure occurrence , with laws distribution such as
Weibull , where an acceleration factor is one parameter .
The 2 types of accelerated tests must be described. HG will make a proposal for the next time.
Development tests by Michel Holy (see attachment 5)
To be seen next meeting
6.3 CEN WG10/EG8
Next meeting :
the § “ review and comparison of environmental management standards” page 39 and
following will be discussed
recommendation for a future work : page 29 ( to confirm)
first part of DEF STAN 0035 and CIN EG 1 ( in English) will be discussed
7- MISCELLANEOUS
- Collin : European Legislation on reducing and/or eliminating lead, cadmium , mercury and
some flame retardants comes into force in July 2006. Collin is making the following 2 parts
proposal :
o The first proposal is for each member of the R and ESS WG. To comment on how
industry in each member country is interpretting and applying the rules of the
legislation
The second proposal is the procurement of lead free components . Are there issues with
reliability ?
- Gunnar arose the subject “ Risk taking relative to guarantee matters” and taking of insurance
in case something goes wrong. He considers that the subject is becoming more serious in the
current context :
o More Virtual testing
o Shorter development time induces shorter testing duration
- Michel Holy points out the fact that the product manufacturer should be responsible in case the
rules of the current state of the art haven’t been followed.See IEC 56 to see if these aspects are
treated.
15 september 2005 page 6/31
8 TOUR OF TABLE
- Colin
60 persons are trained each year by Cranfield/SEE courses in UK
membership has dobbled this year after the campaign
- Gunnar : Unusual number ( 58 , usually 25 ) of participants to a workshop called “ The
breaking point” ; the breaking point is where the virtual testing is taking over from the physical
testing. Exemples were given of electronics designed and tested virtually and brought directly
to the market. We are in fact at the point where the virtual testing plays an increasing role (
50% ? ) and where the physical tests that remain are those which are still necessary.
Programme in English will be sent by Gunnar if available.
- Marco :
o A course on explaining concerns with statistic, uncertainty in the environmental
field
o Sponsoring in march the course of Tustin with LDS
- Helge : project development mechanical and electronic structures for transportation, installation
and use ; 2 or 3 subprojects are defined. Thermal, mechanical , ( EMC ?) all aspects will be
considered. This project will combine previous results achieved in previous projects. It must
help in the design of the products.
- Michel Holy
o The workshop on how to specify the environmental conditions was postpone to
next year
- Henri
o The ASTE guide on ESS based on highly accelerated tests is finished ; see
summary in appendice 7.
15 september 2005 page 7/31
List of virtual members
Current members + following list.
TOOLA Arja NOKIA +358 40 7685072 [email protected]
BODIN Hakan LabTest ? [email protected] ?
STREUBEL Reinhard BGT 49 7551896276 49 7551 892163 [email protected]
TURTOLA Antti KOTEL 358994565639 [email protected]
VAN DORP
Aad National Aerospace
Laboratory
+31-527-248457 +31-527-248210
TURTOLA Antti KOTEL 358994565639 35894567042 [email protected]
15 september 2005 page 8/31
Definition(s) of Terms Dedicated to Availability, Reliability & Maintainability
1) Terminology-Structure
Environment Stress has direct influences on "Reliability" and "Maintainability"
2) Terms of Reliability and their abbreviations
- Reliability Function R(t)
- Failure Rate λ(t) - Mean Time Between Failures MTBF - Mean Time To Failures MTTF - Mean Time To Mission - Failures MTTFM - Lifetime TL - Life Cycle LC - Mission Profile MP - Life Environmental Cycle Profile LCEP
15 september 2005 page 9/31
Durability: capacity of a functional unity to execute a function required in definite conditions of use and
of maintenance till his(its,her) end of useful life or until what it does not agree any more for economical
or technological reasons (ref: Reliability, Maintenabilité and Availability - October, 1993).
- Dependability: together capacities of a product allowing it to arrange functional specified
performances, at the deliberate moment, during duration foreseen, without damage for itself and for its
environment (ref: BNAE RG Aéro 00040).
2.1) Relations between the terms of Reliability
∞
MTTF = ∫R(t)•dt (for Lifetime = ∞)
0
for a finite Lifetime the upper limit of the integral is TL
λ(t) = d R(t) / R(t) •dt
This equation shows that the reliability function R(t) is completely defined by the failurerate λ(t) .
With R(0) = 1, the reliability function reads as follows:
t
- ∫ λ(x) dx
R(t) = e 0
For λ(t) = λ = constant it follows:
∞
R(t) = e- λt
and in this case is MTTF = ∫e- λ(t) dt =1/λ
0
2.2) Terms related to Reliability
Reliability - Analysis - Blockdiagramm - Requirements - Verification - Program - Improvement - Assurance of - Evaluation - Of mechanical Items
15 september 2005 page 10/31
Failure - Failure Analysis - FMEA (Failure Mode And Effects Analysis)
- FMECA (Failure Mode, Effects and Criticality Analysis) - Failure Cause - Failure Mode - Failure Symptom - Failure Criticality - Failure Effect - Failure Detection - Failure Localisation - 8D process
Fault - Specification-fault - Engineering-fault - Manufacturing-fault - Using-fault
Reliability Improvement during
Engineering - R-Verification - R-Analysis - R-Test
- HASS (Highly Accelerated Stress Screening) - HALT (Highly Accelerated Life Testing)
- R-Demonstration
Manufacturing - ESS
- Qualifications-Tests
Product Use - Reliability Growth
3) Terms of Maintainability and their abbreviations
Is there any mathematical presentation of the following terms ?
- Maintenance
- Preventive Maintenance
- Mean Time To Preventive Maintenance MTTPM : no mathematical presentation (i.e. :
valeur moyenne observée)
- Time Between Preventive Maintenance TBPM : no mathematical presentation (i.e. : valeur
moyenne observée)
- Maintenability : Capacity of a product to be put back(handed) in a state of given functioning, in a
specified limit of time (t), when the work is made according to prescribed procedures and given
conditions. This capacity can be translated in the term of probability M (t).
15 september 2005 page 11/31
- Corrective Maintenance
- Mean Time To Repair : MTTR
- Repair Rate µ(t) : Conditional probability that the repairation of a failing product is realized on
an unit of time given from moment t, knowing that it was still not it to t.
3.1) Relations between the terms of Maintainability
to be defined
- µ(t) = d M(t) / M(t) dt (M(t) = maintenability)
- MTTR = = ∫M(t)dt
3.2) Terms related to Maintainability
- Maintainability - Analysis
- Requirements - Verification - Program - Improvement - Assurance of - Evaluation
4) Definitions for Systems and/or Hardware
Functionality
[2] The capability of a product to provide the required function when it is used under specified
conditions.
Operational Availability; Point Availability
[1] Probability that a product will perform its required function under given conditions at a stated
instant of time.
Safety
[1] Ability of a product to cause neither injury to persons, nor significant material damage or other
unacceptable consequences
Remark:
Safety is subdivided into accident prevention (the product is safe working while it is operating
correctly) and technical safety ( the product has to remain safe even if a failure occurs)
15 september 2005 page 12/31
[3] State in which the risk of harm (to persons) or damage is limited to an
acceptable level
Note 1: Safety is one of the aspects of Quality
Note 2: The above definition is valid for the purposes of quality standards. the term "safety" is
defined differently in ISO/IEC Guide 2
Usability
[2] The capability of a product to be understood, learned, used and efficient for the user, when used
under specified conditions.
Operational Effectiveness
Logistical Support
[1] All activities undertaken to provide effective and economical use of an product during ist
operating phase.
Maintainability
[1] Probability that preventive maintenance or repair of an item will be performed within a stated
time interval for given procedures and resources.
Remark:
A qualitative definition is:
Ability of a product to be retained in or restored to the ability to perform its required function in a
given time interval under stated procedures and resources.
Maintainability is subdivided in serviceability (preventive maintenance) and reparability (corrective
maintenance or repair)
Useful Life
[1] Total operating time of a product, ending for a nonrepairable product when the failure probability
becomes too high or the product functionality is obsolete, and for a repairable product when the
intensity of failures becomes unacceptable or when after a failure the product is considered to
be no longer repairable.
Remark:
The term "Life Time" is only used for nonrepairable products. It is the time span between initial
operation and failure of a nonrepairable item.
15 september 2005 page 13/31
Reliability
[1] Probability that a product will perform is required function under given conditions for a stated
time interval.
Remark:
This does not mean that redundant parts may not fail. Such parts can fail and be repaired.
Defect (only used for software)
[1] Nonfulfillment of an intended usage requirement or reasonable expectation, essentially present
at t=0
Remark:
From a technical point of view, a defect is similar to a nonconformity, however not necessarily
from a legal point of view. Defects do not need to influence the item's functionality. They are
caused by flaws (errors, mistakes) during design, production, or installation. Unlike failures,
which always appear in time (generally randomly distributed), defects are present at t=0.
However, some defects can only be detected when the item is operating and are referred to as
"dynamic defects". Similar to defects, with regard to the cause, are systematic failures; they are
not necessarily present at t=0
[3] Nonfulfillment of an intended usage requirement or reasonable expectation, including one
concerned with safety
Note: The expectation must be reasonable under the existing circumstances.
Defect- Immunity) (only used for software)
[2] The capability of the Software product to maintain a level of performance when used under
specified conditions
Note:
Wear or ageing does not occur in software. Limitations in "reliability" are due to faults in
requirements, design, and implementation. "Failures" due to these faults depend on the way the
software product is used and the program options selected rather than on elapsed time.
Supportability, Maintainability ( for software)
[2] The capability of the software product to be modified. Modifications may include corrections,
improvements or adaptation of the software to change in environment, and requirements and
functional specifications.
15 september 2005 page 14/31
Security
[2] The capability of the Software product to protect information and data so that unauthorised
person or systems cannot read or modify them and autorised persons or systems are not
denied access to them.
Failure
[1] Termination of the ability of an item to perform a required function under specified conditions.
Dependability
[1] Collective term used to describe the availability performance and its influencing factors, such as
reliability performance, maintainability performance, and logistical support performance
[3] Collective term used to describe the availability performance and its influencing factors, such as
reliability performance, maintainability performance, and logistical support performance
Note 1: Dependability is used only for general descriptions in non-qualitative terms
Note 2: Dependability is one of the time-related aspects of quality
Note 3: the definition of dependability and note 1 given above are taken from IEC 50(191),
which also includes related terms and definitions.
Functionality ( Capability, Technical Performance)
(1) Ability of an item to meet a service demand of stated quantitative characteristics under given
conditions
(2) The capability of a product to provide the required function when it is used under specified
conditions.
Referenced Documents
[1] A. Birolini, Quality and Reliability of Technical Systems
Springer- Verlag
[2] ISO/IEC 9126-1, Software Engineering - Product Quality Part 1
[3] EN ISO 8402 Quality management and quality assurance - Vocabulary
15 september 2005 page 15/31
1.0 What is a Feasibility Study?
A feasibility study is designed to provide an overview of the primary issues related to
a technical and business idea. The purpose is to identify any "make or break" issues
that would prevent the test from being successful. In other words, a feasibility study
determines whether the technical issues make sense, as well as the business issues
but I am concerned with technical issues here.
A thorough feasibility analysis provides a lot of information necessary for the
technical plan. For example, a good market analysis is necessary in order to
determine whether the project is feasibility. This information provides the basis for the
market section of the business plan.
Because putting together a technical and business plan is a significant investment of
time and money, you want to make sure that there are no major roadblocks facing
you when the test plan is finalized and you make the investment in time and
equipment. Identifying such roadblocks is the purpose of a feasibility study.
A feasibility study looks at three major areas:
1. Market issues (Not dealt with)
2. Organizational/technical issues
3. Financial issues (Not dealt with)
Again, this is meant to be a "first cut" look at these issues. For example, a feasibility
study should not do in-depth long-term financial projections, but it should do a basic
break-even analysis to see how much revenue would be necessary to meet your
operating expenses.
The purpose of the business plan is to minimize the risk associated with a new
business and maximizes the chances of success through research and maximizes
the chances for success through research and planning.
(cf. University of California)
Technological Issues
The cost and availability of technology may be of critical importance to the feasibility
of a project, or it may not be an issue at all.
For example, a service organization, such as a childcare centre, will have a few
equipment and other technology- related issues to address. A manufacturing
15 september 2005 page 16/31
enterprise, on the other hand, may have a number of complex technology questions
to analyze in order to determine whether or not the business is feasible.
Key questions to answer include:
a. What are the technology needs for the proposed business?
b. What other equipment does your proposed business need?
c. Where will you obtain this technology and equipment?
d. When can you get the necessary equipment?
How does your ability to obtain this technology and equipment affect your start-up
timeline?
e. How much will the equipment and technology cost?
Keeping in mind that technology doesn't necessarily mean complex machinery; if
your business simply needs a personal computer, printer, and fax machine, those are
your technological needs.
However, making wise decisions on even simple purchases such as office machines
may require some research. Obviously there are numerous types of personal
computers on the market. You many want to check Consumer Reports for their
recommendations, do some comparative shopping, and ask acquaintances about
their experiences with different companies. Your cost estimates will get plugged into
your financial projections.
Naturally, the more complex the technology you need, the more research that will be
required to make good decisions about it. This is important and should not be looked
at trivially.
Feasible:
“an examination of a situation to decide whether a suggested method, plan or piece
of work is possible or reasonable”.
Feasibility: noun {U}
Whether something is feasible:
"People who consider only price, and not value, are the lawful prey of those who
purvey shoddy goods" John Ruskin (1819 - 1900)
2.0 The Technical Issues to Look at During the Feasibility Study
15 september 2005 page 17/31
In the commercial market we have to decide what we trying to achieve
with a certain test. The main thrust is always the reliability of the
product being manufactured.
The product life cycle begins at the component level and continues through assembly
level; the life cycle includes exposure to the following environments
Assembly/process
Testing
Storage
Transportation
Operating
Servicing ( preventive and corrective maintenance)
2.1.1 Assembly/Process
During processing and assembly of electronic assemblies, temperature excursions
take place, e.g. soldering including reflow, cleaning or imposed thermal cycling tests.
These temperature excursions can be damaging to some parts of the assembly and
consume some part of the available life. This damage should be minimized by
keeping the number of excursions to a minimum and the damage needs to be
considered in the overall reliability estimates.
2.1.2 Testing
When devising the overall reliability test plan the frequency of applied test to the
device and the fatigue that the testing induces into the product will be identified.
2.1.3 Storage
Storage tests will be defined by the product specification. The storage life of the
product will be identified which may range from a few months to many years. A
storage life cycle may include storage in a mobile unit to storage in a temperature-
controlled warehouse.
2.1.4 Transportation
Transportation is not a single event that is simply defined. Each vehicle type may
impose unique environmental loads. Each may also provide protection from certain
environmental conditions. Duration and frequency of occurrence will influence how
15 september 2005 page 18/31
environmental effects are accumulated over time. The
transportation configuration and degree of loading can also
affect the loads imposed on the product.
2.1.5 Operating
It is assumed that the operational characteristics will not affect the reliability test as
the unit is a low power device and operational tests.
2.1.6 Environmental Stress Screening (ESS)
ESS has the potential to identify latent defects that may cause early failures in a
product. ESS needs to be specifically designed to accelerate the failure of 'weak'
elements in the assembly. ESS does not add to the number of such failures but
causes them to occur in a significantly shorter period of time.
Effective ESS programmes should be supported by well planned `Root Cause
Analysis' (RCA) and corrective action resources. These enable timely corrective
actions, elimination of latent defects and ultimate removal of the ESS process subject
to continued monitoring and control of the manufacturing process.
3.0 Conclusion
All the above tests will be scrutinized during a feasibility study, equipment,
infrastructure human resource and all the associated cost that go with these
requirements.
This is the first part in looking at a reliability test programme.
Colin Weetch
15
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pte
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er
20
05
pa
ge
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/31
1
Test obje
ctive (
purp
ose,d
efinitio
n…
) T
est w
here
the a
pp
lied c
on
str
ain
ts r
ose in a
pro
gre
ssiv
e w
ay in v
ery
up
per
valu
es in c
om
parison to
the q
ua
lific
ation s
pecifie
d v
alu
es a
nd
the
essentia
l
obje
ctive o
f w
hic
h b
ein
g t
o investiga
te t
he lim
its o
f
functionin
g a
nd o
f destr
uction o
f th
e p
rod
uct in
ord
er
to
push th
em
aw
ay,
by s
uite
d a
ctions,
in t
he lim
its
imposed b
y t
he s
tate
of
the
art
of
techno
log
y o
f its
constitu
ents
.
2
What is
drivin
g y
ou f
or
perf
orm
ing the test?
-
tim
e to m
ark
et of
the p
roduct
- safe
ty c
onsid
era
tion (
avio
nic
s)
- m
ain
tna
bili
ty c
osts
- te
chno
log
ical lim
it: th
e lim
it o
f re
sis
tance im
posed b
y
the t
echno
log
y o
f a p
rod
uct or
of
a p
art
icula
r
constitu
ent, t
ow
ard
a g
iven
constr
ain
t (t
em
pera
ture
,
vib
ration,
ele
ctr
ic tensio
n,
etc
.). T
his
lim
it e
sta
blis
hes
so a
n u
nbri
dge
ab
le b
arr
ier.
Ex: m
eltin
g p
oin
t of
a
pla
stic b
uild
ing m
ate
rial, te
mpera
ture
the m
axim
um
of a
functionin
g a
sem
iconducto
r in
th
e s
ilico
n, e
lastic lim
it
of
a b
uild
ing
mate
rial, e
tc.
3
Level of
assem
bly
of
the p
roduct subm
itte
d t
o t
est
At th
e lo
west
possib
le le
ve
l of
assem
bly
4
Num
ber
of
item
s s
ubm
itte
d t
o test
The s
tatistical aspects
in r
ela
tion w
ith th
e n
um
ber
of
realiz
ed A
GG
RA
VA
TE
D T
ES
TS
on a
ne
w p
roduct
inte
rven
e to
at
least tw
o le
vels
:
- T
he c
apacity o
f th
e A
GG
RA
VA
TE
D T
ES
TS
to
dis
cover
rele
va
nt causes o
f fa
iling;
- T
he o
bta
inin
g t
he lim
its o
f fu
nctio
nin
g a
nd /
or
of
destr
uctio
n a
nd t
he a
ssocia
ted v
ari
ab
len
ess.
W
ith r
egard
to th
e c
apacity o
f th
e
AG
GR
AV
AT
ED
TE
ST
S to d
iscover
rele
va
nt causes o
f
faili
ng, tw
o c
ases a
re b
e c
onsid
ere
d:
- 1
-st case: th
e r
ele
vant ca
uses o
f fa
iling
Aggra
va
ted
te
sts
15
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pte
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er
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ge
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/31
pre
sum
ed a
re o
f abstr
act n
atu
re a
nd h
ave f
or
eff
ect to
revea
l a
pro
ble
m o
n e
very
cop
y s
ubje
cte
d t
o a
ttem
pt,
sin
ce a
n a
pplie
d c
onstr
ain
t exceeds the
specifie
d
va
lue.
It is tra
nsla
ted g
enera
lly b
y a
n incap
acity o
f
marg
ins, ty
pic
al case o
f th
e u
se o
f a b
adly
ca
libra
ted
constitu
ent. I
n t
hat case,
the r
ealiz
ed
AG
GR
AV
AT
ED
TE
ST
S o
n a
very
lim
ited s
am
ple
of
copie
s, e
ven
on t
he
sin
gle
cop
y, tu
rns o
ut eff
ective to r
eve
al th
e e
xis
tence
of
the r
ele
vant ca
use o
f defe
ct and
po
wer
so to
corr
ect
it.
- 2
-nd c
ase:
the r
ele
va
nt ca
uses o
f fa
ilin
g
pre
sum
ed c
an a
ffect a p
riori o
nly
a w
eak f
raction o
f th
e
com
ple
te p
op
ula
tion o
f th
e p
roduct (f
or
exam
ple
: le
ss
than 5
% o
f th
e p
opu
lation).
In th
at case,
it is n
ot
very
pro
ba
ble
tha
t a lim
ited n
um
ber
of
AG
GR
AV
AT
ED
TE
ST
S a
llow
s t
o r
eve
al th
is r
ele
van
t cause.
As
exam
ple
, th
e u
se o
f th
e m
odel bin
om
ial in
dic
ate
us tha
t
if o
ne h
opes t
o r
evea
l a
n r
ele
vant
cause o
f fa
iling
aff
ecting o
nly
5 %
of
the p
opula
tion w
ith a
pro
bab
ility
of
the s
uccess o
f 80 %
, it w
ou
ld b
e n
ecessary
to
subje
ct
abou
t 30
copie
s to t
he t
est
of
AG
GR
AV
AT
ED
TE
ST
S.
Such q
ua
ntity
is tota
lly inco
mpatible
with
the
im
pera
tive
manufa
ctu
rers
. C
onsequen
tly,
the A
GG
RA
VA
TE
D
TE
ST
S r
ealiz
ed in th
e p
hase o
f conception /
develo
pm
ent on a
n a
lwa
ys v
ery
lim
ited n
um
ber
of
copie
s c
an
not
ha
ve a
gre
at eff
icie
ncy to
ward
the
revea
ling o
f th
is t
ype
of
defe
cts
. O
nly
, a
ggra
vate
d E
SS
(HA
SS
) in
the
ph
ase o
f pro
ductio
n w
ill b
e s
usceptible
to r
evea
l, in a
dd
itio
n t
o th
e m
anufa
ctu
ring d
efe
cts
,
these d
efe
cts
of
the c
oncep
tion
wh
ich w
ould
aff
ect only
a w
eak f
raction o
f th
e p
rod
ucts
durin
g th
eir p
rofile
of
life.
15
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With r
egard
to
the
obta
inin
g the
lim
its o
f fu
nction
ing
and /
or
of
destr
uction o
f th
e p
rod
uct, th
e m
ajo
r
difficulty p
laces its
elf in th
e s
tatistica
l chara
cte
r
associa
ted
to t
hese s
izes.
So, th
e o
bta
inin
g in a
diffe
rent w
ay g
iven v
alu
e o
n the
lim
it o
f fu
nctionin
g th
e
sin
gle
cop
y d
oes n
ot re
vea
l in
evitab
ly th
e c
entr
al va
lue
of
the s
tatistical dis
trib
utio
n o
f th
is lim
it w
hic
h c
ould
be
associa
ted
to a
n im
port
ant
popu
latio
n o
f th
e t
este
d
pro
duct. I
n p
art
icu
lar,
this
unit e
xperim
enta
l va
lue c
an
be a
va
lue o
f ta
il of
dis
trib
ution,
pla
ced t
o th
e left
or
to
the r
ight
of
the d
istr
ibution.
It p
roves w
hy it is
hard
ly
recom
mended,
when it
is c
om
patible
with th
e
impera
tives o
f develo
pm
ent, to m
ake the
AG
GR
AV
AT
ED
TE
ST
S o
n s
evera
l cop
ies a
nd n
ot o
n
the s
ingle
unity. T
he n
um
ber
of
ava
ilab
le c
op
ies b
ein
g
alw
ays v
ery
lim
ited in t
he p
hase o
f de
ve
lopm
ent; o
ne
can c
onsid
er
that a n
um
ber
of
unitie
s w
hic
h a
re a
ble
to
go f
rom
3 to 5
esta
blis
h a
n a
ccepta
ble
com
pro
mis
e.
5
Typ
e o
f pro
duct re
leva
nt to
be s
ubm
itte
d t
o th
e test (
mass v
olu
me lo
w p
rice p
roduct ,..)
1.
Facto
rs b
ou
nd
in
co
sts
an
d in
th
e s
trate
gic
co
nte
xt
"
Str
ate
gic
aspects
bo
und(c
onnecte
d)
to t
he
mark
et (e
x: an
y ri
gh
t fo
r th
e e
rror
from
the lau
nch o
f th
e
firs
t copie
s o
n t
he m
ark
et, m
atu
rity
of
the p
roduct fr
om
the s
tart
ing,
…)
"
The im
pera
tives o
f re
ducin
g the
costs
of
resum
ption o
f th
e d
efe
cts
of
conception
"
The im
pera
tives o
f re
ducin
g the
tim
es o
f
develo
pm
ent
"
The im
pera
tives o
f re
ducin
g the
dura
tio
ns o
f
15
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pte
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ES
S
"
Als
o a
pp
lica
ble
in c
ase o
f chang
e o
f
techno
log
ies if
conditio
ns o
f use a
re c
orr
espond
ing to a
light e
nvironm
ent
"
Hig
h m
ass p
roduction w
ith
weak e
nvironm
enta
l
conditio
ns
"
off
the s
helf e
qu
ipm
ent sub
mitte
to lig
ht
environm
ent in
op
era
tion
2.
bo
un
d(c
on
necte
d)
Facto
rs o
n t
he r
etu
rn t
o
exp
eri
en
ce
(R
EX
)
"
The insuff
icie
nt o
pera
tion
al re
liab
ility
of
sim
ilar
pro
ducts
alread
y d
eve
lop
ed a
nd p
roduced b
y t
he
com
pan
y (
RE
X in
op
era
tion
)
"
Num
ero
us p
roble
ms g
enera
ted in p
rod
uctio
n o
n
sim
ilar
pro
ducts
of
the p
revio
us g
enera
tion
(R
EX
in
pro
duction)
3.
Facto
rs b
ou
nd
to
th
e u
nc
ert
ain
tie
s
"
The u
se o
f te
chno
logie
s in v
ery
in
no
vative
chara
cte
r or
of
the n
ew
str
ate
gie
s o
f im
pla
nting
of
constitu
ents
"
Use o
f ne
w p
rocesses in p
roductio
n
"
The c
onditio
ns o
f em
plo
yment of
the p
rod
uct n
ot
or
little
trie
d
"
Str
on
g v
aria
ble
ness o
f th
e p
rofile
of
use o
f th
e
pro
duct (e
x:
pro
duce
d "
ge
nera
l pu
blic
")
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pte
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"
Str
on
g v
aria
ble
ness o
f th
e p
erf
orm
ances o
r of
chara
cte
ristics o
f th
e p
rod
uct in
som
e c
onstr
ain
ts o
f
environm
ent or
of
use
"
Sup
ply
besid
e n
ew
sup
plie
rs
"
The u
se o
f constitu
ents
except specific
ation (
ex:
the c
ase o
f constitu
ents
" c
ivili
ans "
used in t
he m
ilita
ry
or
spatial app
lica
tio
ns)
6
Test dura
tion
(da
ys,
we
eks, m
onth
s..)
"
The d
ura
tion o
f a a
ggra
vate
d tests
cam
paig
n is
very
bri
ef
: of
the o
rder
of
5 d
ays o
n a
vera
ge
7
Sep
ara
te o
r com
bin
ed e
nvir
onm
ents
C
om
bin
ed e
nvironm
ents
are
not
a c
on
ditio
n b
ut can b
e
em
plo
yed
if
necessary
to d
isclo
se a
failu
re.
For
exam
ple
, w
e c
an g
rad
ually
incre
ase t
he v
ibra
tion
level fo
r a g
ive
n r
ate
of
tem
pera
ture
variatio
n o
r b
y
incre
asin
g g
radu
ally
this
rate
for
a g
ive
n level of
vib
ration.
8
Pro
duct str
ength
an
d e
nvironm
ent str
ess v
aria
bili
ties
are
or
are
n’t c
onsid
ere
d
( in
th
e p
rocess o
f deri
vin
g t
he t
est severity
)
no
9
Does th
e test
brin
g k
now
ledge o
n r
elia
bili
ty p
ara
mete
rs
?
no
10
Does th
e test co
nsum
e tota
lly o
r p
art
ially
the life
pote
ntial ot th
e e
quip
ment subm
itte
d to t
est ?
Yes , t
he p
roduct
und
er
test is
norm
ally
destr
oye
d
11
main
norm
s , s
tandard
s, te
chnic
al re
fere
nces r
ela
tive t
o
this
type
of
tests
no
15
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D
e v e l o p m e n t T e s t
1
Test obje
ctive
(purp
ose,d
efinitio
n…
)
The p
urp
ose o
f accele
ratio
n is to
pro
duce f
ailu
res in a
reasona
ble
tim
e c
om
pare
d to testing a
t n
orm
al conditio
ns.
Form
s o
f accele
rate
d testin
g inclu
de:
−
accele
rate
d s
tress testing,
AS
T, and
−
accele
rate
d life testing,
AL
T
These a
re m
ade to a
sam
ple
of
pro
ducts
to
id
entify
desig
n w
eaknesses a
s the s
cre
en
ing t
ests
are
made to a
ll pro
ducts
in o
rder
to
prim
arily
ide
ntify
weaknesses in m
ate
ria
ls a
nd
pro
cesses.
Anoth
er
typ
e o
f cla
ssific
atio
n o
f accele
rate
d s
tress tests
can b
e m
ade o
n th
e f
ollo
win
g w
ay:
−
tests
that sim
ula
te th
e u
se c
onditio
ns (
"sim
ula
tion t
esting")
– life tests
−
tests
that
aim
at pro
ducin
g f
ailu
res a
nd locating w
eaknesses (
"stim
ula
tio
n testing
") -
accele
rate
d s
tress tests
Accele
rate
d s
tress testing c
an b
e d
efin
ed a
s a
pply
ing h
igh
er
leve
ls o
f str
ess f
or
a s
hort
peri
od
of
tim
e to a
pro
duct un
der
test
assum
ing
it w
ill e
xh
ibit th
e s
am
e f
ailu
re m
echanis
m a
s it w
ould
in
a long
er
am
ount of
tim
e a
t lo
w s
tress le
vels
. T
esting is d
on
e u
ntil fa
ilure
s take
pla
ce a
nd
the
ke
y is
to u
nd
ers
tand t
he f
ailu
res a
nd t
he
ir r
ela
tio
nship
to t
he a
pplie
d s
tresses. T
he s
tress c
onditio
ns a
re n
ot
meant to
accura
tely
rep
lica
te t
he s
tre
ss life c
ycle
in t
he o
pera
tin
g e
nviro
nm
ent but th
e s
tresses a
re a
nyw
ay s
ele
cte
d to
be e
ffective
in
fin
din
g t
he
failu
res in th
e u
se e
nviro
nm
ent.
Accele
rate
d life testing
is p
erf
orm
ed to o
bta
in info
rmation o
n th
e p
roduct (c
om
ponent, m
odule
, syste
m e
tc.)
lifetim
e d
istr
ibution o
r a
part
icu
lar
relia
bili
ty p
ara
mete
r in
a tim
ely
manner.
This
can b
e d
on
e in t
wo d
iffe
rent w
ays
or
in a
com
bin
ation
of
them
:
- usin
g t
ime c
om
pre
ssio
n, fo
r exam
ple
by c
han
gin
g th
e length
of
on a
nd o
ff c
ycle
s
- accele
rating
the
lo
ad
ing c
onditio
ns, th
us d
ecre
asin
g t
he s
afe
ty m
arg
in
The p
urp
ose o
f lif
e testing is to id
entify
th
e r
ele
vant fa
ilure
mechanis
ms that
wo
uld
occur,
and c
orr
ela
te th
ese w
ith t
he p
oin
t in
the
pro
duct’s life t
he f
ailu
re w
ould
occur.
All
the s
tresses d
uring t
he p
rod
uct’s w
hole
life c
ycle
ne
ed t
o b
e a
ddre
ssed –
e.g
. tr
ansport
ation,
sto
rage a
nd t
he a
ctu
al use c
onditio
ns. T
hese c
ond
itio
ns u
sually
inclu
de
diffe
rent and c
ha
ngin
g t
em
pera
ture
s,
hum
idity,
mechanic
al
str
esses (
vib
rations, sh
ock, bum
ps e
tc.)
, ele
ctr
ica
l a
nd e
lectr
om
agnetic p
henom
ena e
tc.
2
What is
drivin
g y
ou
for
perf
orm
ing the
test?
- safe
ty a
nd r
elia
bili
ty c
oncern
s (
avio
nic
s, nucle
ar
etc
.)
-
main
tenance a
nd
gu
ara
nte
e issues
3
Level of
assem
bly
of
the p
roduct
subm
itte
d to t
est
Quite o
ften th
e g
reate
st
be
nefit of
accele
rate
d t
ests
is a
chie
ve
d b
y p
erf
orm
ing tests
at th
e lo
west
level. T
est should
als
o m
e m
ade e
arl
y
in t
he p
roduct
de
velo
pm
ent pro
cess. H
ow
ever,
testing s
hould
be
continu
ed d
uri
ng
the d
iffe
rent phases o
f th
e p
roduct d
evelo
pm
ent –
from
desig
n p
hase (
testing d
one
on e
arl
y p
roto
typ
es)
to m
anufa
ctu
ring q
ualif
icatio
n a
nd p
eri
od
ic q
ualif
ication t
ests
.
4
Num
ber
of
item
s
subm
itte
d to t
est
For
sta
tistica
l confid
ence t
he n
eed is o
ften h
igh
er
than w
hat
is p
ractica
lly p
ossib
le,
abo
ut five b
ein
g a
min
imum
but fe
w tens w
ou
ld b
e
need
ed.
AT
TA
CH
ME
NT
4 a
cce
lera
ted
te
sts
; p
rop
osa
l :
He
lge
Pa
lmen
15
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5
Typ
e o
f pro
duct
rele
vant
to b
e
subm
itte
d to t
he t
est
( m
ass v
olu
me lo
w
price p
roduct ,..)
All
types.
6
Test dura
tion
(da
ys,
weeks, m
onth
s..)
Accele
rate
d s
tress test ca
n b
e m
ade v
aria
bly
in d
ays o
r fe
w w
eeks. Life testing
typic
ally
req
uires s
evera
l w
eeks, even s
om
e m
onth
s.
7
Sep
ara
te o
r
com
bin
ed
environm
ents
Diffe
rent ty
pes o
f str
esses a
re n
eede
d to
pre
cip
itate
th
e d
iffe
rent fa
ilure
mechanis
ms. P
roper
com
bin
ation o
f str
esses m
ay
be u
se
d to
realis
e s
yn
erg
istic e
ffects
– f
or
exam
ple
th
erm
al cyc
ling a
nd v
ibra
tio
n. H
um
idity is a
lso u
sually
ap
plie
d w
ith h
igher
or
vary
ing
tem
pera
ture
.
8
Pro
duct str
ength
an
d
environm
ent str
ess
vari
ab
ilities a
re o
r
are
n’t c
onsid
ere
d
( in
th
e p
rocess o
f
deri
vin
g t
he t
est
severity
)
Yes.
9
Does th
e test
brin
g
know
ledge
on
relia
bili
ty p
ara
mete
rs
?
Life testing a
ims a
t gett
ing a
n e
stim
ate
of
for
exam
ple
of
the f
ailu
re r
ate
(or
MT
TF
, M
TB
F)
or
the o
n-s
et of
we
ar-
out m
echanis
ms (
life
tim
e)
or
at le
ast
the r
ele
va
nt fa
ilure
mechanis
ms.
10
Does th
e test
consum
e tota
lly o
r
part
ially
the life
pote
ntial of
the
equ
ipm
ent subm
itte
d
to test ?
Accele
rate
d s
tress tests
an
d life tests
are
destr
uctive.
11
main
norm
s ,
sta
ndard
s, te
chn
ical
refe
rences r
ela
tive to
this
type
of
tests
- E
nviro
nm
enta
l te
sting
, accele
rate
d s
tress tests
: IE
C 6
0068-2
– s
tandard
series
- M
echan
ica
l an
d c
limatic test m
eth
ods (
sem
iconducto
r devic
es):
IE
C 6
0749
sta
nd
ard
series
15
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/31
1)
Test
ob
jecti
ve
Develo
pm
ent
tests
are
used to
dete
rmin
e th
e ap
titu
de of
com
ponents
, m
ate
rials
and/o
r desig
ns to
m
et
the re
quirem
ents
(f
unctional
an
d en
viro
nm
enta
l) of
a giv
en
specific
atio
n f
or
a n
ew
pro
duct.
2)
Ap
pli
cati
on
The tests
are
do
ne d
urin
g t
he d
evelo
pm
ent and d
esig
n p
hase o
f a p
roje
ct
with
tw
o a
ims:
-
to d
ete
rmin
e the a
bili
ty o
f m
ate
rials
, com
ponents
an
d/o
r desig
ns to r
esis
t on
eff
ects
of
specifie
d e
nviro
nm
enta
l co
nditio
ns,
were
experi
ence is m
issin
g a
nd/o
r ca
lcula
tio
n
or
virtu
al sim
ula
tion is n
ot
possib
le o
r n
ot e
nou
gh a
ccu
rate
. -
to d
ete
rmin
e the a
bili
ty o
f a
desig
n s
olu
tion t
o m
et th
e f
unctio
na
l re
quirem
ents
of
a g
iven
specific
ation.
While
bein
g a
n s
ubsta
ntia
l part
of
develo
pm
ent
costs
and a
n im
port
ant
desig
n t
ool,
it is n
ecessary
to p
lan a
nd t
o b
udg
et
the D
ev
elo
pm
en
t T
ests
at
the v
ery
beg
inn
ing o
f a
develo
pm
ent pro
ject. T
he p
rincip
al in
put fo
r th
is p
lanin
g a
ctivity is th
e p
roduct spe
cific
ation
3)
Kin
d o
f T
est
Regard
ing t
he r
eq
uire
d e
nvironm
enta
l co
nd
itio
ns,
all
kin
ds o
f exis
ting e
nvironm
enta
l T
ests
ma
y b
e u
sed,
but
norm
ally
with
much h
igher
str
ess lim
its t
han t
hose g
iven b
y t
he
specific
atio
n.
The r
ais
on f
or
usin
g h
igh s
tress lim
its is t
o s
pare
test
tim
e a
nd t
o g
et
som
e f
acto
r of
security
re
gard
ing t
he t
est
results.
(HA
ST
: H
ighly
Accele
rate
d S
tress T
est;
HA
LT
: H
ighly
Accele
rate
d L
ifecyc
le T
est)
Outg
oin
g f
rom
the s
pecifie
d e
nviro
nm
enta
l re
qu
irem
ents
rela
ting t
o o
pera
tion,
transport
atio
n a
nd s
tora
ge
, th
e a
ppro
pri
ate
test
pro
ced
ure
s,
the s
tress l
evels
and
the t
est
dura
tion s
hall
be c
hosen
, consid
erin
g th
e e
xperi
ences w
ith e
arl
ier
develo
pm
ent an
d the
know
-ho
w o
f th
e test
specia
lists
.
15
se
pte
mb
er
20
05
pa
ge
27
/31
4)
Test
Co
nd
itio
ns
To a
llow
to d
ete
rmin
e t
he e
ffect
of
sin
gle
str
ess f
acto
rs o
n a
mate
rial or
item
respectively
to a
vo
id t
he r
ecip
rocal in
flu
ence o
f severa
l str
esses,
the t
est
conditio
ns a
re u
sually
specia
l la
b c
on
ditio
ns, not
equa
l to
th
e r
ea
l e
nvironm
enta
l cond
itio
ns o
f th
e p
rod
uct.
Rem
ark
: C
om
bin
ed t
ests
(H
um
idity/T
em
pera
ture
; V
ibra
tion
/Tem
pera
ture
etc
.) a
re a
lso o
ften u
sed,
but
norm
ally
app
lied o
n t
he f
inal
pro
duct
and n
ot
for
the p
urp
ose s
tate
d
out u
nder
1).
5)
Test
Resu
lts
The t
est
results a
re u
sed t
o m
ake d
esig
n d
ecis
ions a
s w
ell
as t
o e
va
luate
the "
Re
liab
ility
" a
nd/o
r th
e "
Life T
ime"
of
a p
rod
uct
an
d t
o p
rove t
he r
ightn
ess o
f a d
esig
n.
There
for
the t
est re
sults, m
eth
ods, to
ols
and c
onditio
ns s
ha
ll b
e d
ocum
ente
d a
nd
sto
red o
n s
uch a
wa
y,
that th
e p
rob
abili
ty o
f lo
osin
g o
r dis
tracting th
en is v
ery
lo
w.
15
se
pte
mb
er
20
05
pa
ge
28
/31
Ac
ce
lera
ted
te
sts
pro
po
sa
l b
y H
en
ri G
rze
sko
wia
k
prin
cip
e
Co
nd
itio
ns o
f a
pp
lica
tio
n
Exp
ecte
d r
esu
lts
Ob
jective
: re
du
ce
th
e te
st
du
ratio
n
Prin
cip
le:
the
p
rod
uct
is su
bje
cte
d to
co
nd
itio
ns
of
use o
r to
co
nstr
ain
ts o
f
en
viro
nm
ent
am
plif
ied
in
o
rde
r to
acce
lera
te
the
m
ech
an
ism
s
of
faili
ng
an
d t
o r
ed
uce
th
e n
ece
ssa
ry d
ura
tion
to
estim
ate
som
e
beh
avio
ral
ch
ara
cte
ristics
of
the
pro
du
ct
in
the
no
rma
l co
nd
itio
ns o
f em
plo
ym
en
t
Kn
ow
th
e
an
aly
tica
l m
ode
l m
akin
g
the
re
latio
n b
etw
ee
n th
e sp
ee
d of
da
ma
ge
w
ith
th
e
am
plit
ud
e
of
the
ap
plie
d c
ond
itio
ns
Kn
ow
th
e
va
lue
of
the
pa
ram
ete
rs
invo
lve
in
th
ese
mo
de
ls
The
pro
vo
ke
d m
ech
anis
ms o
f fa
ilure
ha
ve
to
b
e
rep
rese
nta
tive
of
tho
se
arisin
g in
th
e no
rma
l co
nd
itio
ns of
em
plo
ym
en
t
The
p
hen
om
en
a
of
inte
ractio
ns
be
twe
en
se
ve
ral
co
nstr
ain
ts
of
em
plo
ym
en
t o
r of
en
viro
nm
en
t m
ust
be
ta
ke
n in
to a
ccou
nt.
Eva
lua
tio
n
of
the
be
ha
vio
ral
ch
ara
cte
ristics of
a pro
du
ct
in
the
no
rma
l co
nd
itio
ns
of
em
plo
ym
en
t,
it
for
the
co
mpa
tib
le
pe
rio
ds
with
th
e
ca
len
da
r co
nstr
ain
ts a
sso
cia
ted
to t
he
ph
ase
of
de
ve
lop
men
t of
the
pro
du
ct
15
se
pte
mb
er
20
05
pa
ge
29
/31
__
___
__
__
___
__
__
__
__
___
__
__
__
__
___
__
__
__
__
G
UID
E
En
vir
on
men
tal
Str
ess S
cre
en
ing
fo
r E
lectr
on
ic E
qu
ipm
en
t
usin
g H
igh
ly A
cc
ele
rate
d T
ests
__
___
__
__
___
__
__
__
__
___
__
__
__
__
___
__
__
__
__
January
20
06 E
ditio
n
Mem
bers
of
the A
ST
E E
nvir
onm
enta
l S
tress S
cre
en
ing C
om
mitte
e
havin
g p
art
icip
ate
d in th
e im
ple
menta
tio
n o
f th
is D
ocu
ment
Com
mitte
e P
resid
ent :
Danie
l G
OU
LE
T
T
hale
s D
ivis
ion A
éro
sp
ace
C
om
mitte
e m
em
bers
:
Serg
e B
LA
ZE
JE
WS
KI
Johnson C
ontr
ol
Vin
ce
nt D
ER
OU
ET
F
lextr
on
ics
Fra
ncis
DU
PO
UY
Serm
a T
echnolo
gie
s
Joëlle
DU
SS
AU
LT
A
irb
us
Cla
ude G
IGO
UX
Im
dR
-SD
F
Fabrice G
UE
RIN
IS
TIA
P
hili
pp
e J
EA
NP
IER
RE
E
mitech
Phili
pp
e P
OU
GN
ET
V
alé
o V
EM
S
Jacques R
ING
LE
R
Rin
gle
r C
onsu
ltin
g
Jean M
arie R
OU
RE
V
alé
o V
EC
S / C
EE
Lio
nel S
IMO
N
S
ole
ctr
on
Fré
déric T
RE
NIT
EC
ET
15
se
pte
mb
er
20
05
pa
ge
30
/31
Co
nte
nts
1..
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
In
tro
du
cti
on
an
d h
isto
rical b
ackg
rou
nd
5
2..
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
...
Ob
ject
6
3..
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. D
om
ain
of
ap
plicati
on
6
4..
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. T
erm
ino
log
y
6
5..
....
.. R
em
ind
er
of
the e
nvir
on
men
tal
str
ess s
cre
en
ing
ob
jecti
ves a
nd
pri
ncip
les
7
6..
....
....
....
....
....
....
....
....
....
....
....
. T
he E
SS
op
era
tio
ns a
t vari
ou
s s
tep
s o
f *a
ssem
bly
*
9
6.1
The n
otions o
f hom
og
eneous / h
ete
rog
eneous p
roducts
in fro
nt of
resis
tance t
o c
onstr
ain
ts
9
6.2
....
....
....
....
....
....
....
....
....
....
....
....
...
Incid
ence o
n the testing m
eans s
pecific
ation:
11
7..
....
....
. Ju
sti
ficati
on
of
the “
Hig
hly
accele
rate
d e
nvir
on
men
tal
str
ess s
cre
en
ing
” 1
3
7.1
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
... C
om
parison o
f th
e tw
o m
eth
ods
13
7.1
.1..
....
....
....
....
....
....
.. “
Conventional environm
enta
l str
ess s
cre
enin
g”
meth
od
14
7.1
.2..
....
....
....
....
. “H
ighly
accele
rate
d e
nvironm
enta
l str
ess s
cre
enin
g”
meth
od
16
7.2
....
....
....
....
....
....
....
...
Com
parison o
f th
e e
nvironm
ent str
ess s
cre
enin
g m
eth
ods
18
7.3
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. O
ther
advanta
ges
19
7.4
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. P
ote
ntial pro
ble
ms a
nd p
recautions:
19
8..
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
.. I
nit
ial E
SS
pro
file
set
up
20
8.1
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
...
ES
S p
rofile
phases 2
0
8.2
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. S
ele
ction o
f th
e a
pplic
able
constr
ain
ts:
21
8.3
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
Choic
e o
f th
e E
SS
constr
ain
ts levels
21
8.3
.1..
....
....
....
....
....
....
....
....
....
....
....
...
Fix
ed t
em
pera
ture
s c
ases (
warm
or
cold
)
22
8.3
.2..
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. T
herm
al cycle
s c
ases
24
15
se
pte
mb
er
20
05
pa
ge
31
/31
8.3
.3
Pseudo-u
npre
dic
table
vib
rations c
ases (
3 a
xes, 6 d
eg
rees o
f fr
eedom
) ..
...
27
8.3
.4
Therm
al cycle
s c
om
bin
ed w
ith v
ibra
tions 3
axes 6
deg
rees o
f fr
eedom
: ..
...
28
8.4
....
....
....
....
....
....
....
....
....
....
....
....
.. C
onstr
ain
ts h
arm
lessness o
n s
ound p
roducts
2
9
9..
....
....
....
....
....
....
....
....
....
....
....
...
Ch
ara
cte
risti
cs o
f th
e in
terf
aces u
sed
fo
r th
e E
SS
32
10
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
In
itia
l p
rofi
le a
nd
testi
ng
mean
s v
ali
dati
on
3
3
10.1
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
...
Valid
ation o
f th
e E
SS
harm
lessness
34
10.2
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
.. V
alid
ation o
f th
e E
SS
effic
iency
36
11
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. M
an
ag
em
en
t o
f th
e E
SS
op
era
tio
n
39
11.1
....
....
....
....
....
....
....
.. R
ealis
ation a
nd m
onitoring o
f th
e t
ests
, fa
ilure
s d
ete
ction
39
11.2
....
....
....
....
....
....
....
....
....
....
....
....
....
....
Applic
able
pro
cedure
s in c
ase o
f fa
ilure
s
40
11.3
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. C
apitalis
ation o
f th
e r
esults
40
11.4
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. T
he E
SS
optim
isation
42
12
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
Cli
en
t /
su
pp
lier
inte
rface
12.1
....
....
....
....
....
....
....
....
....
....
....
....
....
. R
esponsib
ilities a
nd c
ontr
actu
al m
odalit
ies
43
12.2
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
. E
SS
pro
file
valid
ation t
ests
synth
esis
4
4
13
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
....
.. B
iblio
gra
ph
ical re
fere
nces
45
Ap
pen
dix
es
Appendix
A:
E
SS
by s
am
plin
g
Appendix
B:
S
om
e o
rders
of m
ag
nitude