Space engineering - Verification

This Standard establishes the requirements for the verification of a space system product.
It defines the fundamental concepts of the verification process, the criteria for defining the verification strategy and specifies the requirements for the implementation of the verification programme. It includes also the list of the expected documentation (i.e. Document requirements definitions, DRDs).
This Standard is intended to apply to different products at different levels from a single equipment to the overall system.
Discipline related verification aspects are complemented in Standards specific to those disciplines.
For verification process for SW the following standards are considered fully sufficient for development of these items:
-   ECSS-E-ST-40 Space engineering - Software
-   ECSS-Q-ST-80 Space product assurance - Software product assurance
Detailed requirements for Testing are covered in the ECSS E-ST-10-03.
This standard does not specifically address Validation of space products as a separate process, since product Verification is performed against requirements that also address the suitability of the product to fulfil the needs of its intended use. As such, Validation is achieved through the Verification process provided adequate requirements are placed on the product.
It is recognised that testing and analysis also occur during the product development process, but they are not addressed by this standard as they are not formal requirement verification activities in the sense of the customer-supplier relationship.
The guidelines on verification are provided in the associated handbook ECSS-E-HB-10-02A.
The requirements on the systems engineering process are gathered in ECSS-E-ST-10 "System Engineering"; specific aspects of the SE process are further elaborated in dedicated standards, in particular: ECSS-E-ST-10-06 "Technical Specification", ECSS-E-ST-10-02 "Verification" (the present standard), and ECSS-E-ST-10-03 "Testing". These standards are based on the same principles, process and documentation model.
The applicability of each these standards can therefore not be considered in isolation from the others
This standard may be tailored for the specific characteristic and constraints of a space project in conformance with ECSS-S-ST-00.

Raumfahrttechnik - Verifikation

Ingénierie spatiale - Vérification

La présente norme définit les exigences applicables à la vérification d'un produit du système spatial.
Elle définit les concepts fondamentaux du processus de vérification, ainsi que les critères pour définir la stratégie de vérification, et spécifie les exigences de mise en oeuvre du programme de vérification. Elle inclut en outre la liste de la documentation attendue (définitions des exigences documentaires ou DRD).
La présente norme est destinée à s'appliquer à différents produits et à différents niveaux, depuis un équipement particulier jusqu’à l'ensemble du système.
Les aspects de la vérification associés à des disciplines particulières sont traités par des normes spécifiques.
Concernant le processus de vérification des logiciels, les normes suivantes sont considérées comme suffisantes pour le développement de ces éléments :
-   ECSS-E-ST-40 Ingénierie spatiale - Logiciels
-   ECSS-Q-ST-80 Assurance produit des projets spatiaux - Assurance produit logiciel
Les exigences d'essai détaillées sont décrites dans l'ECSS E-ST-10-03.
La présente norme ne traite pas de manière spécifique de la validation des produits spatiaux en tant que processus distinct, car la vérification des produits est effectuée en fonction d'exigences liées à la capacité du produit à satisfaire les besoins associés à son utilisation prévue. C'est pourquoi la validation est effectuée dans le cadre du processus de vérification, sous réserve que le produit s'accompagne des exigences appropriées.
Il est admis que les essais et analyses interviennent également au cours du processus de développement du produit. Ils ne sont cependant pas traités dans la présente norme, dans la mesure où ils ne sont pas considérés comme des activités formelles de vérification des exigences au sens de la relation client-fournisseur.
Les lignes directrices relatives à la vérification sont fournies dans le manuel associé ECSS-E-HB-10-02A.
Les exigences relatives au processus d'ingénierie des systèmes sont réunies dans l'ECSS-E-ST-10, « Ingénierie système » ; les aspects spécifiques au processus d'IS sont décrits de façon plus détaillée dans des normes dédiées, à savoir : ECSS-E-ST-10-06 « Spécification technique de besoin », ECSS-E-ST-10-02 « Vérification » (la présente norme) et ECSS-E-ST-10-03 « Vérification par essai ». Ces normes se fondent sur les mêmes principes, les mêmes processus et le même modèle de documentation.
L'applicabilité de chacune de ces normes ne peut donc être envisagée de manière indépendante.
La présente norme peut être adaptée aux caractéristiques et contraintes spécifiques d'un projet spatial conformément à l'ECSS-S-ST-00.

Vesoljska tehnika - Preverjanje

Ta standard določa zahteve za preverjanje izdelka vesoljskega sistema.
Opredeljuje temeljne koncepte postopka preverjanja, merila za določanje strategije preverjanja in določa zahteve za izvajanje programa preverjanja. Vključuje tudi seznam pričakovane dokumentacije (tj. dokumente z definicijami zahtev, DRD-je).
Ta standard se uporablja za različne izdelke na različnih ravneh od posameznega kosa opreme do celotnega sistema.
Vidiki preverjanja, povezani s posamezno disciplino, so dopolnjeni s standardi, specifičnimi za te discipline.
V okviru postopka preverjanja programske opreme naslednji standardi povsem zadostujejo za razvoj teh postavk:
– ECSS-E-ST-40 Vesoljska tehnika - Programska oprema
– ECSS-Q-ST-80 Zagotavljanje varnih proizvodov v vesoljski tehniki - Zagotavljanje varne programske opreme
Podrobne zahteve za preskušanje so zajete v standardu ECSS E-ST-10-03.
Ta standard se posebej ne nanaša na preverjanje vesoljskih izdelkov v smislu ločenega procesa, saj se preverjanje izdelkov izvaja glede na zahteve, ki obravnavajo tudi primernost izdelka za izpolnitev potreb njegove predvidene uporabe. Preverjanje se tako izvaja s postopkom preverjanja, v katerem mora izdelek izpolnjevati ustrezne zahteve.
Znano je, da se preskušanje in analiza izvajata tudi med procesom razvoja izdelka, vendar ju ta standard ne zajema, ker nista formalni dejavnosti preverjanja zahtev v smislu razmerja med stranko in dobaviteljem.
Smernice za preverjanje so navedene v pripadajočem priročniku ECSS-E-HB-10-02A.
V standardu ECSS-E-ST-10 »Sistemski inženiring« so zajete zahteve za postopek sistemskega inženiringa; posebni vidiki postopka sistemskega inženiringa so natančneje določeni v namenskih standardih, točneje: ECSS-E-ST-10-06 »Tehnična specifikacija«, ECSS-E-ST-10-02 »Preverjanje« (ta standard) in ECSS-E-ST-10-03 »Preskušanje«. Navedeni standardi temeljijo na enakih načelih, procesu in modelu dokumentiranja.
Zato uporabnosti posameznega standarda ni mogoče presojati ločeno od ostalih standardov.
Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.

General Information

Status
Published
Publication Date
27-Nov-2018
Withdrawal Date
30-May-2019
Technical Committee
Drafting Committee
Current Stage
9060 - Closure of 2 Year Review Enquiry - Review Enquiry
Start Date
03-Jun-2024
Completion Date
03-Jun-2024

Relations

Effective Date
05-Dec-2018

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SLOVENSKI STANDARD
01-februar-2019
1DGRPHãþD
SIST EN 14725:2004
Vesoljska tehnika - Preverjanje
Space engineering - Verification
Raumfahrttechnik - Verifikation
Ingénierie spatiale - Vérification
Ta slovenski standard je istoveten z: EN 16603-10-02:2018
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 16603-10-02
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2018
ICS 49.140
Supersedes EN 14725:2003
English version
Space engineering - Verification
Ingénierie spatiale - Vérification Raumfahrttechnik - Verifikation
This European Standard was approved by CEN on 28 September 2018.

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,
Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.

CEN-CENELEC Management Centre:
Rue de la Science 23, B-1040 Brussels
© 2018 CEN/CENELEC All rights of exploitation in any form and by any means Ref. No. EN 16603-10-02:2018 E
reserved worldwide for CEN national Members and for
CENELEC Members.
Table of contents
European Foreword . 4
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. 9
3.4 Nomenclature . 9
4 Verification principles . 10
4.1 Verification process . 10
4.1.1 Verification objectives . 10
4.1.2 Verification activities . 10
4.1.3 Verification documentation . 11
4.2 Verification planning . 12
4.2.1 Verification approach . 12
4.2.2 Verification methods . 12
4.2.3 Verification levels . 12
4.2.4 Verification stages . 13
4.2.5 Model philosophy . 13
4.2.6 Verification tools . 13
4.3 Verification execution and reporting . 13
4.4 Verification control and closeout . 13
5 Verification requirements . 14
5.1 Verification process . 14
5.2 Verification planning . 14
5.2.1 Verification approach . 14
5.2.2 Verification methods . 15
5.2.3 Verification levels . 17
5.2.4 Verification stages . 17
5.2.5 Models . 19
5.2.6 Verification tools . 19
5.2.7 Verification process phasing . 20
5.2.8 Verification planning documents. 21
5.3 Verification execution and reporting . 22
5.3.1 General . 22
5.3.2 Verification execution and reporting documentation . 22
5.4 Verification control and close-out . 24
5.4.1 General . 24
5.4.2 Verification control board (VCB) . 24
5.4.3 Re-verification . 25
5.4.4 Verification control and close-out documentation . 26
6 Pre-tailoring matrix per space product types . 27
Annex A (normative) Verification plan (VP) - DRD . 36
Annex B (normative) Verification control document (VCD) - DRD . 39
Annex C (normative) Test report - DRD . 42
Annex D (normative) Review-of-design report - DRD . 44
Annex E (normative) Inspection report - DRD . 46
Annex F (normative) Verification report - DRD . 48
Bibliography . 50

Figures
Figure 4-1: Verification process and activities . 11

Tables
Table 5-1: Product categories according to heritage . 18
Table 6-1: Definitions of the columns of Table 6-2 . 28
Table 6-2: Pre-tailoring matrix per “Space product types” . 29

European Foreword
This document (EN 16603-10-02:2018) has been prepared by Technical Committee CEN/CLC/TC 5
“Space”, the secretariat of which is held by DIN (Germany).
This document (EN 16603-10-02:2018) originates from ECSS-E-ST-10-02C Rev.1.
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 May 2019, and conflicting national standards shall be
withdrawn at the latest by May 2019.
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 14725:2003.
The main differences between EN 14725:2003 (that was based on ECSS-E-10-02A) and this standard
are:
• Restructuring of the document following, in particular: moving of the guidelines in the
associated Handbook, inclusion of an introductive clause on the Verification principles,
structuring of the requirement clauses in line with the verification process flow as
summarized in the principles.
• Clarification on standard applicability to different types of products (e.g. launcher,
transportation system, ground segment, GSE).
• Clarification of the verification vs. validation coverage.
• Moving of detailed test requirements to EN 16603-1003 (based on ECSS-E-ST-10-03C)
“Testing” including AIT Plan, Test Specification and Test Procedure DRDs.
• Introduction of risk assessment and mitigation plan concerning those requirements not
verified by test.
• Clarification on the applicability of verification by similarity as analysis method in
relationship to different types of products (requirement 5.2.2.3c)
• Clarification on product categories vs. heritage and relevant qualification requirements (clause
5.2.4.2)
• Clarification on in-orbit stage verification activities, in particular the relationship with the
commissioning (clause 5.2.4.5)
• Inclusion of a requirement concerning the verification database delivery in electronic form
(requirement 5.4.1c)
• Introduction of “status of compliance” in the VCD data (VCD DRD)
• Simplification of DRD’s number and content
This document has been prepared under a standardization request 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, Serbia, Slovakia, Slovenia,
Spain, Sweden, Switzerland, Turkey and the United Kingdom.
Scope
This Standard establishes the requirements for the verification of a space system
product.
It defines the fundamental concepts of the verification process, the criteria for
defining the verification strategy and specifies the requirements for the
implementation of the verification programme. It includes also the list of the
expected documentation (i.e. Document requirements definitions, DRDs).
This Standard is intended to apply to different products at different levels from
a single equipment to the overall system.
Discipline related verification aspects are complemented in Standards specific
to those disciplines.
For verification process for SW the following standards are considered fully
sufficient for development of these items:
• ECSS-E-ST-40 Space engineering – Software
• ECSS-Q-ST-80 Space product assurance - Software product assurance
Detailed requirements for Testing are covered in the ECSS E-ST-10-03.
This standard does not specifically address Validation of space products as a
separate process, since product Verification is performed against requirements
that also address the suitability of the product to fulfil the needs of its intended
use. As such, Validation is achieved through the Verification process provided
adequate requirements are placed on the product.
It is recognised that testing and analysis also occur during the product
development process, but they are not addressed by this standard as they are
not formal requirement verification activities in the sense of the customer-
supplier relationship.
The guidelines on verification are provided in the associated handbook ECSS-E-
HB-10-02A.
The requirements on the systems engineering process are gathered in ECSS-E-
ST-10 “System Engineering”; specific aspects of the SE process are further
elaborated in dedicated standards, in particular: ECSS-E-ST-10-06 “Technical
Specification”, ECSS-E-ST-10-02 “Verification” (the present standard), and
ECSS-E-ST-10-03 “Testing”. These standards are based on the same principles,
process and documentation model.
The applicability of each these standards can therefore not be considered in
isolation from the others
This standard may be tailored for the specific characteristic and constraints 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 revision of any of these publications
do not
...

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