Space engineering - Mechanical - Part 1: Thermal control

EN 14607 Part 1 of Space engineering - Mechanical specifies requirements for the discipline of thermal engineering.
This document specifies the requirements for the definition, analysis, design, manufacture, verification and in­service operation of thermal control subsystems of spacecraft and other space products.
This document applies to the thermal engineering activities of all spacecraft and space related products for all thermal aspects and temperature levels for space products.
For this document, the complete temperature scale is divided into three ranges defined as follows:
- Cryogenic temperature range, below 120 K;
- Conventional temperature range, between 120 K and 420 K;
- High temperature range, above 420 K.
The core part of this document concerns the conventional temperature range; complementary information, requirements and definitions for the cryogenic and high temperature range respectively are provided in annexes B and C.
When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project.
NOTE   Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements.
This document is applicable to:
- thermal engineering activities of all space and space related products, covering all thermal engineering aspects involved in the achievement of the required thermal performance, particularly: design, verification, manufacturing and in service operations;
- thermal control subsystem and to relevant parts of all space products.

Raumfahrttechnik - Mechanik - Teil 1: Thermalkontrolle

Ingénierie spatiale - Mécanique - Partie 1: Contrôle thermique

Vesoljska tehnika – Mehanika – 1. del: Nadzor toplote

General Information

Status
Withdrawn
Publication Date
03-Aug-2004
Withdrawal Date
20-Jan-2026
Technical Committee
CEN/SS T02 - Aerospace
Drafting Committee
CEN/SS T02 - Aerospace
Current Stage
9960 - Withdrawal effective - Withdrawal
Start Date
24-Sep-2014
Completion Date
28-Jan-2026

Relations

Effective Date
08-Jun-2022
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026

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Frequently Asked Questions

EN 14607-1:2004 is a standard published by the European Committee for Standardization (CEN). Its full title is "Space engineering - Mechanical - Part 1: Thermal control". This standard covers: EN 14607 Part 1 of Space engineering - Mechanical specifies requirements for the discipline of thermal engineering. This document specifies the requirements for the definition, analysis, design, manufacture, verification and in­service operation of thermal control subsystems of spacecraft and other space products. This document applies to the thermal engineering activities of all spacecraft and space related products for all thermal aspects and temperature levels for space products. For this document, the complete temperature scale is divided into three ranges defined as follows: - Cryogenic temperature range, below 120 K; - Conventional temperature range, between 120 K and 420 K; - High temperature range, above 420 K. The core part of this document concerns the conventional temperature range; complementary information, requirements and definitions for the cryogenic and high temperature range respectively are provided in annexes B and C. When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project. NOTE Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements. This document is applicable to: - thermal engineering activities of all space and space related products, covering all thermal engineering aspects involved in the achievement of the required thermal performance, particularly: design, verification, manufacturing and in service operations; - thermal control subsystem and to relevant parts of all space products.

EN 14607 Part 1 of Space engineering - Mechanical specifies requirements for the discipline of thermal engineering. This document specifies the requirements for the definition, analysis, design, manufacture, verification and in­service operation of thermal control subsystems of spacecraft and other space products. This document applies to the thermal engineering activities of all spacecraft and space related products for all thermal aspects and temperature levels for space products. For this document, the complete temperature scale is divided into three ranges defined as follows: - Cryogenic temperature range, below 120 K; - Conventional temperature range, between 120 K and 420 K; - High temperature range, above 420 K. The core part of this document concerns the conventional temperature range; complementary information, requirements and definitions for the cryogenic and high temperature range respectively are provided in annexes B and C. When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project. NOTE Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements. This document is applicable to: - thermal engineering activities of all space and space related products, covering all thermal engineering aspects involved in the achievement of the required thermal performance, particularly: design, verification, manufacturing and in service operations; - thermal control subsystem and to relevant parts of all space products.

EN 14607-1:2004 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.

EN 14607-1:2004 has the following relationships with other standards: It is inter standard links to EN 16603-31:2014, EN 13291-3:2003, EN 13291-2:2003, EN 13701:2001, EN 13290-5:2001, EN 14725:2003, EN ISO 14620-1:2002. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 14607-1:2004 is associated with the following European legislation: Standardization Mandates: M/237. 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.

EN 14607-1:2004 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.

Standards Content (Sample)


2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika – Mehanika – 1. del: Nadzor toploteRaumfahrttechnik - Mechanik - Teil 1: ThermalkontrolleIngénierie spatiale - Mécanique - Partie 1: Contrôle thermiqueSpace engineering - Mechanical - Part 1: Thermal control49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 14607-1:2004SIST EN 14607-1:2005en01-januar-2005SIST EN 14607-1:2005SLOVENSKI
STANDARD
SIST EN
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