SIST EN 14607-1:2005

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• Status: Withdrawn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: 31-Dec-2004
• Withdrawal Date: 01-Dec-2014
• ICS: 49.140 - Space systems and operations
• Technical Committee: SS SPL - Technical Board for the general field
• Current Stage: 9900 - Withdrawal (Adopted Project)
• Start Date: 01-Dec-2014
• Due Date: 24-Dec-2014
• Completion Date: 02-Dec-2014
• Mandate: M/237 - Mandate to CEN, CENELEC and ETSI for standardization in the field of equipment for the space industry
• Ref Project: EN 14607-1:2004 - Space engineering - Mechanical - Part 1: Thermal control

Relations

• Replaced By: SIST EN 16603-31:2015 - Space engineering - Thermal control general requirements
• Effective Date: 01-Jan-2015
• Replaced By: SIST EN 16603-31:2015 - Space engineering - Thermal control general requirements
• Effective Date: 08-Jun-2022

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
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