EN 16603-35-01:2014
(Main)Space engineering - Liquid and electric propulsion for spacecraft
Space engineering - Liquid and electric propulsion for spacecraft
This Standard defines the regulatory aspects applicable to elements and processes for liquid, including cold gas, and electrical propulsion for spacecraft. It specifies the activities to be performed in the engineering of such propulsion systems, their applicability, and defines the requirements for the engineering aspects: functional, interfaces, environmental, design, quality factors, operational and verification.
General requirements applying to all type of Propulsion Systems Engineering are defined in ECSS-E-ST-35.
This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
Raumfahrttechnik - Flüssige und elektrische Antriebe von Raumfahrzeugen
Ingénierie spatiale - Propulsion liquide et électrique pour satellites
La présente Norme définit les aspects réglementaires applicables aux éléments et aux techniques de propulsion liquide, y compris à gaz froid, et électrique pour engins spatiaux. Elle stipule les activités devant être exécutées dans le cadre de l'ingénierie de tels systèmes de propulsion, ainsi que leur applicabilité, et définit les exigences concernant les aspects liés à l'ingénierie : aspects fonctionnels, interfaces, aspects environnementaux, conception, facteurs de qualité, aspects opérationnels et vérification.
Les exigences générales qui s'appliquent à tous les types d'ingénierie de systèmes de propulsion sont définies dans l'ECSS-E-ST-35.
La présente norme peut être adaptée aux caractéristiques et contraintes spécifiques d'un projet spatial, conformément à la norme ECSS-S-ST-00.
Vesoljska tehnika - Pogon za vesoljska plovila
Standard EN 16603-35-01 določa regulatorne vidike, ki veljajo za elemente in postopke za tekočine, vključno s hladnim plinom in električnim pogonom za vesoljska plovila. Določa dejavnosti, ki se izvajajo v tehničnem delu teh pogonskih sistemov, in njihovo uporabnost ter zahteve za tehnične vidike: funkcionalne, vmesniške, okoljske, zasnovne in kakovostne dejavnike, zahteve med delovanjem in verifikacijo. Splošne zahteve, ki veljajo za vse vrste inženiringa pogonskih sistemov, so opredeljene v standardu ECSS-E-ST-35. 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 - Pogon za vesoljska plovilaRaumfahrttechnik - Flüssige und elektrische Antriebe von RaumfahrzeugenIngénierie spatiale - Propulsion liquide et électrique pour satellitesSpace engineering - Liquid and electric propulsion for spacecraft49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 16603-35-01:2014SIST EN 16603-35-01:2014en,fr,de01-november-2014SIST EN 16603-35-01:2014SLOVENSKI
STANDARDSIST EN 14607-5-1:20051DGRPHãþD
SIST EN 16603-35-01:2014
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-35-01
September 2014 ICS 49.140
Supersedes EN 14607-5-1:2004 English version
Space engineering - Liquid and electric propulsion for spacecraft
Ingénierie spatiale - Propulsion liquide et électrique pour satellites
Raumfahrttechnik - Flüssige und elektrische Antriebe von Raumfahrzeugen This European Standard was approved by CEN on 23 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 16603-35-01:2014 E
SIST EN 16603-35-01:2014
EN 16603-35-01:2014 (E) 2 Table of contents Foreword . 5 Introduction . 6 1 Scope . 7 2 Normative references . 8 3 Terms, definitions and abbreviated terms . 9 3.1 Terms from other standards . 9 3.2 Abbreviated terms. 9 4 Liquid propulsion systems for spacecraft . 10 4.1 Overview . 10 4.2 Functional . 10 4.2.1 Mission . 10 4.2.2 Functions . 11 4.3 Constraints . 11 4.3.1 Accelerations . 11 4.3.2 Pressure vessels and pressurized components . 12 4.3.3 Induced and environmental temperatures . 12 4.3.4 Thermal fluxes . 12 4.3.5 Thruster plume effects . 12 4.4 Interfaces . 12 4.5 Design . 13 4.5.1 General .
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