SIST EN 16602-60-14:2015
(Main)Space product assurance - Relifing procedure - EEE components
Space product assurance - Relifing procedure - EEE components
This standard specifies the requirements, also known as “relifing requirements”, for the planned, intentional storage, control, and removal from storage of electronic, electrical and electromechanical parts which are intended to be used for space applications.
The relifing process is a lot quality control activity. The inspections and tests defined do not constitute an up-screening or up-grading of components to a higher level of quality than procured to.
This standard is applicable to all EEE parts covered by ECSS-Q-ST-60 and used in space programmes.
This standard is not applicable to naked dice.
This standard does not cover the relifing of commercial parts.
Raumfahrtproduktsicherung - Wiederbelebungsprozeduren für EEE-Komponenten
Assurance produit des projets spatiaux - Procédure de déstockage - Composants EEE
Zagotavljanje varnih proizvodov v vesoljski tehniki - Postopek oživljanja komponent EEE
Ta standard določa zahteve, znane tudi kot »zahteve za oživljanje«, za načrtovano, namerno shranjevanje, nadzor in prekinitev shranjevanja elektronskih, električnih in elektromehanskih delov, ki so namenjeni vesoljskim uporabam. Postopek oživljanja je dejavnost nadzora kakovosti serije. Opredeljeni pregledi in preskusi ne predstavljajo presejanja ali izboljšanja komponent, da se doseže višja raven kakovosti od naročene. Ta standard velja za vse dele EEE iz standarda ECSS-Q-ST-60, ki se uporabljajo v vesoljskih programih. Ta standard se ne uporablja za elemente, ki se dobavljajo brez ovoja oziroma ohišja. Ta standard ne obravnava oživljanja komercialnih delov.
General Information
Relations
Standards Content (Sample)
SLOVENSKI STANDARD
SIST EN 16602-60-14:2015
01-januar-2015
Zagotavljanje varnih proizvodov v vesoljski tehniki - Postopek oživljanja
komponent EEE
Space product assurance - Relifing procedure - EEE components
Raumfahrtproduktsicherung - Wiederbelebungsprozeduren für EEE-Komponenten
Assurance produit des projets spatiaux - Procédure de déstockage - Composants EEE
Ta slovenski standard je istoveten z: EN 16602-60-14:2014
ICS:
49.140 Vesoljski sistemi in operacije Space systems and
operations
SIST EN 16602-60-14:2015 en,fr,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
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SIST EN 16602-60-14:2015
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SIST EN 16602-60-14:2015
EUROPEAN STANDARD
EN 16602-60-14
NORME EUROPÉENNE
EUROPÄISCHE NORM
September 2014
ICS 49.140
English version
Space product assurance - Relifing procedure - EEE
components
Assurance produit des projets spatiaux - Procédure de Raumfahrtproduktsicherung - Wiederbelebungsprozeduren
déstockage - Composants EEE für EEE-Komponenten
This European Standard was approved by CEN on 13 March 2014.
CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving
this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning
such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN and CENELEC
member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation
under the responsibility of a CEN and CENELEC member into its own language and notified to the CEN-CENELEC Management Centre
has the same status as the official versions.
CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium, Bulgaria,
Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece,
Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia,
Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.
CEN-CENELEC Management Centre:
Avenue Marnix 17, B-1000 Brussels
© 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved Ref. No. EN 16602-60-14:2014 E
worldwide for CEN national Members and for CENELEC
Members.
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SIST EN 16602-60-14:2015
EN 16602-60-14:2014 (E)
Table of contents
Foreword . 4
1 Scope . 5
2 Normative references . 6
3 Terms, definitions and abbreviated terms . 7
3.1 Terms from other standards . 7
3.2 Terms and definitions specific to the present standard . 7
3.3 Abbreviated terms. 11
3.4 Symbols . 11
4 Environmental parameters for storage . 12
4.1 General rules and requirements. 12
4.1.1 Introduction . 12
4.1.2 Procedures . 12
4.1.3 Storage area and storage zone . 12
4.1.4 Cleanliness . 12
4.1.5 ESD protection . 13
4.1.6 Packing – Packaging – Handling . 13
4.1.7 Quality assurance requirements for storage areas . 13
4.2 Storage conditions . 13
4.2.1 Air . 13
4.2.2 Temperature . 13
4.2.3 Relative humidity (RH) . 14
4.2.4 Package . 14
5 Timing parameters . 15
6 Control parameters . 16
6.1 Test requirements . 16
6.1.1 General requirements per EEE parts family: . 16
6.1.2 Specific requirements per EEE parts family:. 16
6.1.3 Electrical testing . 18
6.1.4 External visual inspection . 18
2
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EN 16602-60-14:2014 (E)
6.1.5 Seal test . 18
6.2 Nonconformance . 18
6.3 Relifing datecode . 19
6.4 Relifing report . 19
6.5 Certificate of Conformity . 19
Annex A (normative) Relifing report - DRD . 22
Annex B (informative) ESD . 25
Bibliography . 28
Figures
Figure 3-1: Timing parameters . 10
Figure A-1 : Example of a relifing traveller sheet . 24
Tables
Table 5-1: Timing parameters. 15
Table 6-1: Control parameters and detailed application of categories . 19
Table B-1 : ESD classes . 27
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EN 16602-60-14:2014 (E)
Foreword
This document (EN 16602-60-14:2014) has been prepared by Technical Committee
CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN.
This standard (EN 16602-60-14:2014) originates from ECSS-Q-ST-60-14C.
This European Standard shall be given the status of a national standard, either by
publication of an identical text or by endorsement, at the latest by March 2015,
and conflicting national standards shall be withdrawn at the latest by March
2015.
Attention is drawn to the possibility that some of the elements of this document
may be the subject of patent rights. CEN [and/or CENELEC] shall not be held
responsible for identifying any or all such patent rights.
This document has been prepared under a mandate given to CEN by the
European Commission and the European Free Trade Association.
This document has been developed to cover specifically space systems and has
therefore precedence over any EN covering the same scope but with a wider
domain of applicability (e.g. : aerospace).
According to the CEN-CENELEC Internal Regulations, the national standards
organizations of the following countries are bound to implement this European
Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic,
Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France,
Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia,
Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom.
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SIST EN 16602-60-14:2015
EN 16602-60-14:2014 (E)
1
Scope
This standard specifies the requirements, also known as “relifing requirements”,
for the planned, intentional storage, control, and removal from storage of
electronic, electrical and electromechanical parts which are intended to be used
for space applications.
The relifing process is a lot quality control activity. The inspections and tests
defined do not constitute an up-screening or up-grading of components to a
higher level of quality than procured to.
This standard is applicable to all EEE parts covered by ECSS-Q-ST-60 and used in
space programmes.
This standard is not applicable to naked dice.
This standard does not cover the relifing of commercial parts.
5
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EN 16602-60-14:2014 (E)
2
Normative references
The following normative documents contain provisions which, through reference
in this text, constitute provisions of this ECSS Standard. For dated references,
subsequent amendments to, or revision of any of these publications do not apply,
However, parties to agreements based on this ECSS Standard are encouraged to
investigate the possibility of applying the more recent editions of the normative
documents indicated below. For undated references, the latest edition of the
publication referred to applies.
EN reference Reference in text Title
EN 16601-00-01 ECSS-S-ST-00-01 ECSS system – Glossary of terms
EN 16602-10-09 ECSS-Q-ST-10-09 Space product assurance – Nonconformance control
system
EN 16602-60 ECSS-Q-ST-60 Space product assurance – Electrical, electronic and
electromechanical (EEE) components
EN 16602-70-01 ECSS-Q-ST-70-01 Space product assurance – Cleanliness and
contamination control
ESCC 24900 Minimum Requirements for Controlling
Environmental Contamination of Components
IPC/JEDEC J-STD-033 Standard for Handling, Packing, Shipping and Use of
Moisture/ re-flow Sensitive Surface Mount Devices
July 2002 version A
ESCC 20600 Preservation, Packaging and dispatch of SCC
Electronic Components
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EN 16602-60-14:2014 (E)
3
Terms, definitions and abbreviated terms
3.1 Terms from other standards
For the purpose of this Standard, the terms and definitions from ECSS-S-ST-00-01
and ECSS-Q-ST-60 apply.
For the purposed of this Standard the following terms from ECSS-Q-ST-70-01
apply:
clean area
cleanroom
3.2 Terms and definitions specific to the present standard
3.2.1 antistatic material
material that minimizes the generation of static charges
NOTE 1 This term refers to the reduction of triboelectric
charge generation.
NOTE 2 This property is not dependent upon material
resistivity.
3.2.2 conductive material
material with the following characteristics:
surface conductive type: materials with a surface resistivity less than
5
10 Ω/.
volume conductive type: materials with a volume resistivity less
4
than 10 Ω-cm.
3.2.3 contaminant
unwanted molecular or particulate matter (including microbiological matter) on
the surface or in the environment of interest that can affect or degrade the
relevant performance or life time
3.2.4 container
receptacle which holds, restrains or encloses an item
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3.2.5 (original) date code
code used by the EEE part manufacturer at assembly step that indicates the
production date
NOTE 1 Generally four-figure codes; two for the year and
two for the week.
NOTE 2 Special lot number can also identify the date
code.
3.2.6 (relifing) date code:
code indicating the date an item is submitted to relifing
NOTE Four-figure code, two for the year and two for
the week.
3.2.7 dissipative material
material with the following characteristics:
surface conductive type: materials with a surface resistivity equal to
5 12
or greater than 10 Ω/ but less than 10 Ω/.
volume conductive type: materials with a volume resistivity equal to
4 11
or greater than 10 Ω-cm but less than 10 Ω-cm.
3.2.8 electrostatic charge
negative or positive electrical charge present on the material or item surface, at
rest
3.2.9 electrostatic discharge (ESD)
transfer of electrostatic charge between objects at different potentials caused by
direct contact or induced by an electrostatic field
3.2.10 electrostatic discharge sensitive (ESDS)
tendency of the performance of EEE parts to be affected or damaged by an ESD
event
3.2.11 ESD protected area
area which is constructed and equipped with the necessary ESD protective
materials, equipment, and procedures, to limit ESD voltages below the sensitivity
level of ESDS items handled therein
3.2.12 ESD protective material
material with one or more of the following properties: limits the generation of
electrostatic charge, dissipates electrostatic charge, and provides shielding from
electric fields
3.2.13 ESD protective packaging
packaging with ESD protective materials to prevent ESD damage to ESDS items
3.2.14 electrostatic shield
barrier or enclosure that prevents or attenuates the penetration of an electric field
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3.2.15 handled or handling
actions during which items are hand manipulated or machine processed
3.2.16 identification
application of appropriate markings to ensure that the identity of an item is
unfailingly indicated after preservation and each stage of packing
3.2.17 isolating material
material not defined as conductive or dissipative are
considered to be isolating
3.2.18 package
support used for enveloping, protecting or containing materials
NOTE Different types of packages are normally used:
Primary, intermediate and final packages
3.2.19 (primary) package
container, envelope or wrap holding an individual item
3.2.20 (intermediate) package
container holding two or more primary packages
3.2.21 (final) package
container holding one or more intermediate packages, used for transportation of
supplies to the orderer
3.2.22 packaging
operations consisting in the preparation of supplies for transit and delivery.
NOTE The term includes preservation, identification
and packing
3.2.23 packing
operation by which supplies are placed in container or wrapped and placed in
containers
3.2.24 particle
unit of matter with observable length, width and thickness
NOTE A particle can be object of solid or liquid
composition, or both, and generally between
0,001 μm and 1000 μm in size
3.2.25 preservation
cleaning of a item and the application of a suitable temporary protective, where
necessary, to maintain the item in prime condition
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3.2.26 relifing procedures
set of tests performed on an item previously stored to verify that its initial quality
and reliability have not been affected by time
3.2.27 storage area
area in the storage site where EEE parts are stored and which contains one or
more storage zones.
3.2.28 storage long duration
storage for which duration exceeds 3 years
3.2.29 storage site
geographical location where EEE parts are stored for a short, medium or long
term period
NOTE For this site the requirements given in this
standard apply: EEE parts manufacturer’s
premises, procurement Agency, EEE part user.
3.2.30 storage zone
defined space in which EEE parts are stored and which is equipped for the
monitoring and the control of storage conditions.
3.2.31 timing parameters
One of the following parameters:
o T0 : Original date code
o T1 : Maximum allowed storage period from T0 with no relifing
control
o T2 : Maximum duration between the original date code of part and its
mounting
o T3 : Maximum allowed storage period after a relifing control.
T3
T2
T1
T0
Figure 3-1: Timing parameters
3.2.32 triboelectric effect
generation of electrostatic charge on an object by rubbing or other type of contact.
10
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EN 16602-60-14:2014 (E)
3.3 Abbreviated terms
For the purpose of this Standard, the abbreviated terms from ECSS-S-ST-00-01
and the following apply:
Abbreviation Meaning
application specific integrated circuit
ASIC
charge coupled device
CCD
charge device model
CDM
destructive physical analysis
DPA
digital signal processor
DSP
electronic, electrical and electromechanical
EEE
European space components coordination
ESCC
electrostatic discharge
ESD
field programmable gate arrays
FPGA
human body model
HBM
joint electronic devices engineering council
JEDEC
machine model
MM
microwave monolithic integrated circuit
MMIC
not applicable
NA
nonconformance report
NCR
national space agency
NSA
relative humidity
RH
space components steering board
SCSB
very large scale integration
VLSI
3.4 Symbols
Ω
ohm
Ω/ ohm per square
Ω-cm
ohm centimetre
μm micrometer
V
volt
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EN 16602-60-14:2014 (E)
4
Environmental parameters for storage
4.1 General rules and requirements
4.1.1 Introduction
This clause defines the rules for storing EEE parts used on space programs.
Those rules are in line with the requirements defined in ESCC Basic Specification
24900.
4.1.2 Procedures
a. The following domains shall be covered and documented by procedures
sent to the customer for information, on request:
1. Storage area and storage zone
2. Cleanliness
3. ESD protection
4. Packing and Packaging
5. Handling
6. Quality assurance.
4.1.3 Storage area and storage zone
a. It shall be demonstrated that storage areas and storage zones provide such
protection against vibration, electromechanical fields, radiation fields and
against light so that possible degradation of organic packaging material is
prevented.
4.1.4 Cleanliness
a. Rules for cleanliness efficiency shall be implemented.
b. The working areas and the contained equipment shall be maintained as
visually clean with no loose material.
c. Access rules shall apply for personnel, materials and equipment.
d. Storage areas shall conform to a cleanliness level as defined in ECSS-Q-ST-
70-01 clause 5.3.1.4.
NOTE This cleanliness level is often called and known
as “grey zone”.
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SIST EN 16602-
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