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.
General Information
Relations
Overview
SIST EN 16603-31:2015 - Space engineering: Thermal control general requirements (adopted from ECSS‑E‑ST‑31) defines the engineering and programmatic requirements for spacecraft and launcher thermal control subsystems (TCS). The standard covers the full lifecycle: definition, analysis, design, manufacture, verification and in‑service operation of TCS across the full temperature scale, divided into cryogenic, conventional, and high temperature ranges. It is applicable to all flight hardware of space projects and may be tailored in conformance with ECSS‑S‑ST‑00.
Key topics and technical requirements
The standard lays out requirements and guidance for thermal engineering at system and unit levels, including:
- Mission and phase-driven requirements
- Consideration of ground, pre‑launch, launch/ascent, orbital/planetary, interplanetary, docking, entry/landing and post‑landing phases.
- Performance requirements
- Thermal functionality and range coverage for cryogenic, conventional and high temperature regimes.
- Interface and subsystem requirements
- Requirements toward mechanical, electrical, AOCS, TM/TC, OBDH, launcher interfaces, GSE and ECLS.
- Design considerations
- Budget allocation, parts/materials/processes (PMP), EEE component constraints, lifetime, predictability, testability, reliability, maintenance, safety and interchangeability.
- Verification and test
- Overview of verification approach for TCS, with specific emphasis on thermal verification and Thermal Balance Test (TBT).
- Production, QA and in‑service
- Procurement, manufacturing process controls, quality management, contamination control, integration, handling, storage and repair.
- Deliverables and documentation
- Hardware deliverables, required documentation and mathematical models; Document Requirements Definitions (DRD) list is provided.
- Annexes
- Annex G and Annex H summarize requirements specific to the cryogenic and high temperature ranges.
Practical applications and users
SIST EN 16603-31:2015 is intended for:
- Thermal engineers and subsystem designers defining TCS architectures and thermal budgets.
- Systems engineers integrating thermal requirements with mechanical, electrical and AOCS disciplines.
- Spacecraft and launcher manufacturers, suppliers and integrators responsible for production and verification.
- Test laboratories planning thermal balance and qualification testing.
- Project managers, procurement and product assurance teams using the DRD and deliverable checklists to ensure compliance.
- Organizations tailoring ECSS standards for specific mission constraints.
Related standards and notes
- Originated from ECSS‑E‑ST‑31 (ECSS‑E‑ST‑31C) and published as EN 16603‑31:2014, adopted by national body as SIST EN 16603‑31:2015.
- Supersedes EN 14607‑1:2004 and integrates with ECSS system‑level tailoring rules (ECSS‑S‑ST‑00).
Keywords: thermal control, spacecraft thermal control, thermal engineering, thermal verification, thermal balance test, cryogenic thermal, high temperature thermal, ECSS, SIST EN 16603‑31:2015.
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
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
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Frequently Asked Questions
SIST EN 16603-31:2015 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Space engineering - Thermal control general requirements". This standard covers: 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.
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.
SIST EN 16603-31:2015 is classified under the following ICS (International Classification for Standards) categories: 49.140 - Space systems and operations. The ICS classification helps identify the subject area and facilitates finding related standards.
SIST EN 16603-31:2015 has the following relationships with other standards: It is inter standard links to SIST EN 14607-1:2005. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 16603-31:2015 is associated with the following European legislation: Standardization Mandates: M/496. When a standard is cited in the Official Journal of the European Union, products manufactured in conformity with it benefit from a presumption of conformity with the essential requirements of the corresponding EU directive or regulation.
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