EN 16602-70-04:2014
(Main)Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies
Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies
This Standard establishes the requirements for the specification, the procedures, the execution and the reporting of a thermal cycling test under vacuum for the evaluation of materials, processes, mechanical parts and assemblies intended for use in the fabrication of spacecraft and associated equipment. This is one of the tests to determine the ability of theses articles to withstand changes of ambient temperature under vacuum.
Typical materials or assemblies that can be evaluated by means of this test method are listed below.
• adhesives;
• adhesive bonded joints;
• coatings (paint, thermal and protective);
• insulating materials;
• metallic bonded joints;
• metallic samples, finished by plating or chemical conversion;
• metallized plastic films;
• organic or non‐organic bonding;
• plated surfaces;
• potting compounds;
• reinforced structural laminates;
• sealants.
NOTE This is not an exhaustive list and other products or items can be tested.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS‐S‐ST‐00.
Raumfahrtproduktsicherung - Temperaturtest zur Untersuchung von Werkstoffen, Prozessen, mechanischen Teilen und Zusammenbauten der Raumfahrttechnik
Assurance produit des projets spatiaux - Essais thermiques pour l’évaluation des matériaux, des processus, des composants et assemblages mécaniques d'un projet spatial
Zagotavljanje varnih proizvodov v vesoljski tehniki - Toplotno preskušanje za ocenjevanje vesoljskih materialov, procesov, mehanskih delov in sestavov
Ta standard določa zahteve za specifikacijo, postopke, izvedbo in poročanje o toplotnem cikličnem preskusu pod vakuumom za ocenjevanje materialov, procesov, mehanskih delov ter sestavov, namenjenih uporabi pri izdelovanju vesoljskih plovil in povezane opreme. To je eden od preskusov za ugotavljanje sposobnosti teh izdelkov za prenašanje sprememb temperature okolice pod vakuumom. Običajni materiali ali sestavi, ki jih je mogoče oceniti s to preskusno metodo, so navedeni spodaj: • lepila; • z lepilom povezani spoji; • premazi (barvni, toplotni in zaščitni); • izolacijski materiali; • kovinski povezani spoji; • kovinski vzorci, dokončani z obdelavo površine ali kemijsko reakcijo; • metalizirani plastični filmi; • organsko ali anorgansko povezovanje; • obdelane površine; • spojine za zapolnjevanje; • okrepljeni strukturni laminati; • tesnilne mase. OPOMBA: To ni izčrpen seznam, pri čemer je mogoče preskusiti druge proizvode ali elemente. Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS‐S‐ST‐00.
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Standards Content (Sample)
SLOVENSKI STANDARD
01-januar-2015
1DGRPHãþD
SIST EN 14098:2004
Zagotavljanje varnih proizvodov v vesoljski tehniki - Toplotno preskušanje za
ocenjevanje vesoljskih materialov, procesov, mehanskih delov in sestavov
Space product assurance - Thermal testing for the evaluation of space materials,
processes, mechanical parts and assemblies
Raumfahrtproduktsicherung - Temperaturtest zur Untersuchung von Werkstoffen,
Prozessen, mechanischen Teilen und Zusammenbauten der Raumfahrttechnik
Assurance produit des projets spatiaux - Essais thermiques pour l’évaluation des
matériaux, des processus, des composants et assemblages mécaniques d'un projet
spatial
Ta slovenski standard je istoveten z: EN 16602-70-04:2014
ICS:
49.140 Vesoljski sistemi in operacije Space systems and
operations
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD
EN 16602-70-04
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2014
ICS 49.140 Supersedes EN 14098:2001
English version
Space product assurance - Thermal testing for the evaluation of
space materials, processes, mechanical parts and assemblies
Assurance produit des projets spatiaux - Essais thermiques Raumfahrtproduktsicherung - Temperaturtest zur
pour l'évaluation des matériaux, des processus, des Untersuchung von Werkstoffen, Prozessen, mechanischen
composants et assemblages mécaniques d'un projet Teilen und Zusammenbauten der Raumfahrttechnik
spatial
This European Standard was approved by CEN on 20 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 16602-70-04:2014 E
worldwide for CEN national Members and for CENELEC
Members.
Table of contents
Foreword . 4
Introduction . 5
1 Scope . 6
2 Normative references . 7
3 Terms, definitions and abbreviated terms . 8
3.1 Terms from other standards . 8
3.2 Terms specific to the present standard . 8
3.3 Abbreviated terms. 8
4 Principles . 9
5 Requirements . 11
5.1 Specifying test . 11
5.1.1 General provision . 11
5.1.2 Specifying the test means . 11
5.1.3 Specifying the thermal cycling test procedures . 12
5.2 Preparing and performing Test . 13
5.2.1 General . 13
5.2.2 Preparing the item to be tested . 13
5.2.3 Preparing the facilities and equipment. 14
5.2.4 Running the thermal cycling test procedures . 14
5.3 Recording and reporting the test results . 15
5.3.1 Test records . 15
5.3.2 Test report . 16
5.3.3 Acceptance criteria and nonconformance . 16
Annex A (normative) Request for thermal cycling test - DRD . 17
Annex B (normative) Thermal cycling test specifications and procedures
(Work Proposal) - DRD . 18
Annex C (normative) Thermal cycling test report - DRD . 19
Annex D (informative) Thermal cycling test procedures . 20
Annex E (informative) Thermal cycling test equipment . 23
Bibliography . 24
Figures
Figure 4-1: Thermal cycling test process overview . 9
Figure D-1 : Test procedure flow diagram . 22
Foreword
This document (EN 16602-70-04:2014) has been prepared by Technical
Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN.
This standard (EN 16602-70-04:2014) originates from ECSS-Q-ST-70-04C.
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 April 2015,
and conflicting national standards shall be withdrawn at the latest by April
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 supersedes EN 14098:2001.
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.
Introduction
The deleterious effects to be anticipated during the thermal cycling test under
vacuum include:
• outgassing,
• cracking or fracture of materials or assemblies due to sudden
dimensional changes by expansion,
• contraction or pressure,
• short circuiting of electrical wiring,
• overheating of materials or assemblies due to change in convection and
conductive heat transfer characteristics.
Scope
This Standard establishes the requirements for the specification, the procedures,
the execution and the reporting of a thermal cycling test under vacuum for the
evaluation of materials, processes, mechanical parts and assemblies intended
for use in the fabrication of spacecraft and associated equipment. This is one of
the tests to determine the ability of theses articles to withstand changes of
ambient temperature under vacuum.
Typical materials or assemblies that can be evaluated by means of this test
method are listed below.
• adhesives;
• adhesive bonded joints;
• coatings (paint, thermal and protective);
• insulating materials;
• metallic bonded joints;
• metallic samples, finished by plating or chemical conversion;
• metallized plastic films;
• organic or non-organic bonding;
• plated surfaces;
• potting compounds;
• reinforced structural laminates;
• sealants.
NOTE This is not an exhaustive list and other products
or items can be tested.
This standard may be tailored for the specific characteristic and constrains of a
space project in conformance with ECSS-S-ST-00.
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 revisions 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 most 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 16602-20 ECSS-Q-ST-20 Space product assurance – Quality assurance
EN 16602-20-07 ECSS-Q-ST-20-07 Space product assurance – Quality assurance for test
centres
EN 16602-70 ECSS-Q-ST-70 Space product assurance – Materials, mechanical
parts and processes
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-70 apply.
3.2 Terms specific to the present standard
3.2.1 batch
see “lot”
3.2.2 lot
quantity produced at one operation
NOTE 1 One lot can be divided in several sub-lots.
NOTE 2 The term “batch” is synonymous.
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
quartz crystal microbalance
QCM
ultraviolet
UV
Principles
The principles of the thermal test for the evaluation of space materials and
processes is to submit the item to be tested (materials, processes, mechanical
parts or assemblies) to a certain number of thermal cycles, oscillating within an
defined temperature range in order to anticipate and to evaluate the resistance
to deleterious effects as:
• outgassing,
• cracking or fracture of materials or assemblies due to sudden
dimensional changes by expansion,
• contraction or pressure,
• short circuiting of electrical wiring,
• overheating of materials or assemblies due to change in convection and
conductive heat transfer characteristics.
For this purpose the activities related to thermal cycling tests requirements,
specifications, procedures and reports are described in Figure 4-1 and the
related requirements are captured in clause 5.
Request for Thermal Work Proposal for Thermal Test (including test
Test (Annex A) specification and procedure (Annex B)
Clause 5.1
Specifying test
Go/NO Go from Customer
Thermal Test results (including
Clause 5.2
identified deviations, if any)
Quality Requirements
Preparing and
performing test
NCR (if any identified
deviation)
Clause 5.3
Recording and
Thermal Test ing
reporting test
Report (Annex C)
Figure 4-1: Thermal cycling test process overview
Clause 5.1 provides the specification for the means and procedures of tests
(facilities, equipments and special apparatus) and the item to be tested.
Clause 5.2 and 5.3 provide the requirements for preparing, performing,
recording and reporting a thermal cycling test.
Requirements
5.1 Specifying test
5.1.1 General provision
a. The customer shall provide a request for thermal test in conformance
with the DRD in Annex A.
b. ECSS-Q-ST-20 shall be made applicable in the request for thermal cycling
test.
c. ECSS-Q-ST-10-09 shall be made applicable in the request for thermal
cycling test.
d. For safety and security, the test centre shall comply with ECSS-Q-ST-20-
07, clause 9.
NOTE Examples of safety issues are “hazard” and
“health”. An example for security issues is
“access control”.
e. The supplier shall provide a thermal cycling test proposal in
conformance with the DRD in Annex B for customer app
...
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