EN 16603-20-06:2014
(Main)Space engineering - Spacecraft charging
Space engineering - Spacecraft charging
This standard is a standard within the ECSS hierarchy. It forms part of the electrical and electronic engineering discipline (ECSS-E-ST-20) of the engineering branch of the ECSS system (ECSS-E). It provides clear and consistent provisions to the application of measures to assess, in order to avoid and minimize hazardous effects arising from spacecraft charging and other environmental effects on a spacecraft’s electrical behaviour.
This standard is applicable to any type of spacecraft including launchers, when above the atmosphere.
Although spacecraft systems are clearly subject to electrical interactions while still on Earth (e.g. lightning and static electricity from handling), these aspects are not covered, since they are common to terrestrial systems and covered elsewhere. Instead this standard covers electrical effects occurring in space (i.e. from the ionosphere upwards).
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Raumfahrttechnik - Aufladung von Raumfahrzeugen
Ingénierie spatiale - Charges électrostatique des véhicules spatiaux
La présente norme s'inscrit dans la hiérarchie ECSS. Elle est rattaché à la discipline « génie électrique et électronique » (ECSS-E-ST-20) de la branche ingénierie du système ECSS (ECSS-E). Elle contient des dispositions claires et cohérentes relatives à l'application de mesures visant à prévenir et minimiser les effets dangereux associés à la charge électrostatique des engins spatiaux, ainsi que les autres effets environnementaux sur le comportement électrique d'un engin spatial.
Cette norme s'applique à tout type d'engin spatial, y compris les lanceurs, au-dessus de l'atmosphère terrestre.
Bien que les systèmes d'engins spatiaux soient clairement soumis à des interactions électriques lorsqu'ils sont au sol (par exemple, éclair et électricité statique pendant la manutention), ces aspects ne sont pas couverts par la présente norme puisqu'ils sont communs aux systèmes terrestres et font l'objet d'autres publications. La présente norme s'attache plus particulièrement aux effets électriques survenant dans l'espace (c'est-à-dire au-delà de l'ionosphère).
La présente norme peut être adaptée aux caractéristiques et contraintes spécifiques d'un projet spatial conformément à l'ECSS-S-ST-00.
Vesoljska tehnika - Napajanje vesoljskih plovil
Standard EN 16603-20-06 je standard v okviru hierarhije ECSS. Je del discipline električnega in elektronskega načrtovanja (ECSS-E-ST-20) veje načrtovanja sistema ECSS (ECSS-E). Zagotavlja jasne in skladne določbe za uporabo ukrepov za oceno, da bi se preprečili in čim bolj zmanjšali nevarni vplivi, ki izhajajo iz napajanja vesoljskih plovil, in drugi okoljski vplivi na električno obnašanje vesoljskega plovila. Ta standard se uporablja za vse vrste vesoljskih plovil, vključno z napravami za izstrelitev, ko so nad atmosfero. Čeprav na sisteme vesoljskih plovil, ko so še na Zemlji, seveda vplivajo električne motnje (npr. strela in statična elektrika zaradi ravnanja), ti vidiki niso obravnavani, saj so skupni zemeljskim sistemom in so obravnavani v drugih standardih. Namesto tega ta standard obravnava električne učinke, do katerih prihaja v vesolju (tj. od ionosfere navzgor). 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)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika - Napajanje vesoljskih plovilRaumfahrttechnik - Aufladung von RaumfahrzeugenIngéniérie spatiale - Charges électrostatique des vehicules spatialesSpace engineering - Spacecraft charging49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 16603-20-06:2014SIST EN 16603-20-06:2014en01-september-2014SIST EN 16603-20-06:2014SLOVENSKI
STANDARD
SIST EN 16603-20-06:2014
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-20-06
July 2014 ICS 49.140
English version
Space engineering - Spacecraft charging
Ingéniérie spatiale - Charges électrostatique des vehicules spatiales
Raumfahrttechnik - Aufladung von Raumfahrzeugen 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 16603-20-06:2014 E SIST EN 16603-20-06:2014
EN 16603-20-06:2014 (E) 2 Table of contents Foreword . 9 Introduction . 10 1 Scope . 12 2 Normative references . 13 3 Terms, definitions and abbreviated terms . 14 3.1 Terms defined in other standards . 14 3.2 Terms specific to the present standard . 14 3.3 Abbreviated terms. 17 4 Overview . 19 4.1 Plasma interaction effects . 19 4.1.1 Presentation . 19 4.1.2 Most common engineering concerns . 19 4.1.3 Overview of physical mechanisms . 20 4.2 Relationship with other standards . 22 5 Protection programme . 24 6 Surface material requirements . 25 6.1 Overview . 25 6.1.1 Description and applicability . 25 6.1.2 Purpose common to all spacecraft . 26 6.1.3 A special case: scientific spacecraft with plasma measurement instruments . 26 6.2 General requirements . 26 6.2.1 Maximum permitted voltage . 26 6.2.2 Maximum resistivity .
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