Space engineering - Electromagnetic compatibility

EMC policy and general system requirements are specified in ECSS-E-ST-20.
This ECSS-E-ST-20-07 Standard addresses detailed system requirements (Clause 4), general test conditions, verification requirements at system level, and test methods at subsystem and equipment level (Clause 5) as well as informative limits (Annex A).
Associated to this standard is ECSS-E-ST-20-06 “Spacecraft charging”, which addresses charging control and risks arising from environmental and vehicle-induced spacecraft charging when ECSS-E-ST-20-07 addresses electromagnetic effects of electrostatic discharges.
Annexes A to C of ECSS-E-ST-20 document EMC activities related to ECSS E ST 20 07: the EMC Control Plan (Annex A) defines the approach, methods, procedures, resources, and organization, the Electromagnetic Effects Verification Plan (Annex B) defines and specifies the verification processes, analyses and tests, and the Electromagnetic Effects Verification Report (Annex C) document verification results. The EMEVP and the EMEVR are the vehicles for tailoring this standard.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.

Raumfahrttechnik - Elektromagnetische Kompabilität

Ingéniérie spatiale - Compatibilité électromagnétique

Les principes de CEM et les exigences générales applicables au système sont spécifiés dans l'ECSS-E-ST-20.
Cette norme ECSS-E-ST-20-07 spécifie les exigences détaillées applicables au système (article 4), les conditions générales d'essai, les exigences de vérifications au niveau système et les méthodes d'essai aux niveaux sous-systèmes et équipements (article 5) ainsi que les limites données à titre d'information (Annexe A).
L'ECSS-E-ST-20-06 « Charge de l'engin spatial » est associée à la présente norme. Elle traite du contrôle de la charge et des risques provenant de la charge de l'engin spatial induite par l'environnement et le véhicule, tandis que l'ECSS-E-ST-20-07 traite des effets électromagnétiques des décharges électrostatiques.
Les annexes A à C de l'ECSS-E-ST-20 documentent les activités CEM liées à l'ECSS E ST 20 07 : le plan de contrôle CEM (annexe A) définit l'approche, les méthodes, les procédures, les ressources et l'organisation ; le plan de vérification des effets électromagnétiques (annexe B) définit et spécifie les processus de vérification, les analyses et les essais, enfin le rapport de vérification des effets électromagnétiques (annexe C) documente les résultats de vérification. EMEVP et EMEVR constituent le moyen de mise en place de la présente norme.
La présente norme peut être adaptée aux caractéristiques et contraintes spécifiques d'un projet spatial conformément à l'ECSS-S-ST-00.

Vesoljska tehnika - Elektromagnetna združljivost

Politika glede elektromagnetne združljivosti in splošne sistemske zahteve so opredeljene v standardu ECSS-E-ST-20. Ta standard ECSS-E-ST-20-07 obravnava podrobne sistemske zahteve (točka 4), splošne preskusne pogoje, pogoje glede preverjanja na sistemski ravni in preskusne metode na ravni podsistemov in opreme (točka 5) ter tudi informativne omejitve (dodatek A). S tem standardom je povezan standard ECSS-E-ST-20-06 o napajanju vesoljskih plovil, ki obravnava nadzor nad polnjenjem in tveganja, ki izhajajo iz okoljskega napajanja vesoljskih plovil ter napajanja, ki ga sproži vozilo, medtem ko standard ECSS-E-ST-20-07 obravnava elektromagnetne učinke elektrostatičnih praznitev. Dodatki A do C standarda ECSS-E-ST-20 beležijo dejavnosti v zvezi z elektromagnetno združljivostjo, povezane s standardom ECSS-E-ST-20-07: načrt obvladovanja elektromagnetne združljivosti (dodatek A) določa pristop, metode, postopke, vire in organizacijo, načrt za preverjanje elektromagnetnih učinkov (dodatek B) določa in opredeljuje procese, analize in preskuse v zvezi s preverjanjem, poročilo o preverjanju elektromagnetnih učinkov (dodatek C) pa beleži rezultate preverjanja. Načrt za preverjanje elektromagnetnih učinkov in poročilo o preverjanju elektromagnetnih učinkov služita za prilagajanje tega standarda. Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.

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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika - Elektromagnetna združljivostRaumfahrttechnik - Elektromagnetische KompabilitätIngéniérie spatiale - Compatibilité électromagnétiqueSpace engineering - Electromagnetic compatibility49.140Vesoljski sistemi in operacijeSpace systems and operations33.100.01Elektromagnetna združljivost na splošnoElectromagnetic compatibility in generalICS:Ta slovenski standard je istoveten z:EN 16603-20-07:2014SIST EN 16603-20-07:2014en01-oktober-2014SIST EN 16603-20-07:2014SLOVENSKI

SIST EN 16603-20-07:2014

EN 16603-20-07
July 2014 ICS 49.140
English version
Space engineering - Electromagnetic compatibility
Ingéniérie spatiale - Compatibilité électromagnétique
Raumfahrttechnik - Elektromagnetische Kompabilität This European Standard was approved by CEN on 10 February 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 worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16603-20-07:2014 E SIST EN 16603-20-07:2014

EN 16603-20-07:2014 (E) 2 Table of contents Foreword . 6 Introduction . 7 1 Scope . 8 2 Normative references . 9 3 Terms, definitions and abbreviated terms . 10 3.1 Terms from other standards . 10 3.2 Terms specific to the present standard . 11 3.3 Abbreviated terms. 13 4 Requirements . 15 4.1 General system requirements . 15 4.2 Detailed system requirements . 15 4.2.1 Overview . 15 4.2.2 EMC with the launch system . 15 4.2.3 Lightning environment . 16 4.2.4 Spacecraft charging and effects . 16 4.2.5 Spacecraft DC magnetic emission . 17 4.2.6 Radiofrequency compatibility . 18 4.2.7 Hazards of electromagnetic radiation . 18 4.2.8 Intrasystem EMC . 18 4.2.9 EMC with ground equipment . 19 4.2.10 Grounding . 19 4.2.11 Electrical bonding requirements . 20 4.2.12 Shielding (excepted wires and cables) .

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