SIST EN 16603-31:2015
(Main)Space engineering - Thermal control general requirements
Space engineering - Thermal control general requirements
ECSS-E-ST-31 defines requirements for the discipline of thermal engineering.
This Standard defines the requirements for the definition, analysis, design, manufacture, verification and in-service operation of thermal control subsystems of spacecraft and other space products.
For this Standard, the complete temperature scale is divided into three ranges:
• Cryogenic temperature range
• Conventional temperature range
• High temperature range.
The requirements of this Standard are applicable to the complete temperature scale. However, where applicable, requirements are stated to be applicable only for the cryogenic or high temperature range. References to these specific requirements have been summarized in Annex G and Annex H.
This standard is applicable to all flight hardware of space projects, including spacecraft and launchers.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Raumfahrttechnik - Thermalkontrolle, allgemeine Andorderungen
Ingénierie spatiale - Contrôle thermique, exigences générales
Vesoljska tehnika - Nadzor toplote, splošne zahteve
Standard ECSS-E-ST-31 določa zahteve za toplotno tehniko. Ta standard določa zahteve za definicijo, analizo, zasnovo, izdelavo, preverjanje in obratovanje toplotnih nadzornih podsistemov vesoljskih plovil in drugih vesoljskih proizvodov. Za ta standard se popolna temperaturna lestvica razdeli na tri območja: • območje kriogenskih temperatur, • območje običajnih temperatur, • območje visokih temperatur. Zahteve iz tega standarda se uporabljajo za popolno temperaturno lestvico. Vendar se, kadar je to primerno, zahteve uporabljajo le za območje kriogenskih ali visokih temperatur. Sklicevanja na te specifične zahteve so povzeta v dodatkih G in H. Ta standard se uporablja za vso letalsko strojno opremo vesoljskih projektov, vključno z vesoljskimi plovili in lansirniki. 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 - Nadzor toplote, splošne zahteveRaumfahrttechnik - Thermalkontrolle, allgemeine AndorderungenIngénierie spatiale - Contrôle
thermique, exigences généralesSpace engineering - Thermal control general requirements49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 16603-31:2014SIST EN 16603-31:2015en,fr,de01-januar-2015SIST EN 16603-31:2015SLOVENSKI
STANDARDSIST EN 14607-1:20051DGRPHãþD
SIST EN 16603-31:2015
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-31
September 2014 ICS 49.140
Supersedes EN 14607-1:2004
English version
Space engineering - Thermal control general requirements
Ingénierie spatiale - Contrôle
thermique, exigences générales
Raumfahrttechnik - Thermalkontrolle, allgemeine Andorderungen This European Standard was approved by CEN on 1 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 worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16603-31:2014 E
SIST EN 16603-31:2015
EN 16603-31:2014 (E) 2 Table of contents Foreword . 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. 19 4 Requirements . 21 4.1 Mission . 21 4.1.1 General . 21 4.1.2 Ground and pre-launch . 21 4.1.3 Launch and ascent . 21 4.1.4 Planetary orbital phases . 22 4.1.5 Interplanetary phases . 22 4.1.6 Planetary natural environment . 22 4.1.7 Docking, docked and separation phases . 22 4.1.8 Descent, entry and landing . 23 4.1.9 Post-landing phases . 23 4.2 Performance . 23 4.2.1 General . 23 4.2.2 High temperature range . 24 4.2.3 Cryogenic temperature range . 24 4.2.4 Functionality . 25 4.3 Requirements towards other subsystems . 25 4.3.1 General . 25 4.3.2 Mechanical . 25 4.3.3 Electrical . 26 4.3.4 AOCS. 26 4.3.5 TM/TC . 27 SIST EN 16603-31:2015
EN 16603-31:2014 (E) 3 4.3.6 OBDH and S/W . 27 4.3.7 Launcher . 27 4.3.8 GSE . 28 4.3.9 ECLS . 28 4.4 Design . 28 4.4.1 General . 28 4.4.2 Budget allocation . 29 4.4.3 Parts, materials and processes (PMP) . 29 4.4.4 EEE components . 29 4.4.5 Lifetime . 29 4.4.6 Predictability and testability . 29 4.4.7 Fl
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