Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft

EN 14607 Part 5.1 of Space engineering - Mechanical defined the requirements for the discipline liquid and electric propulsion for spacecraft
This document belongs to the propulsion field of the mechanical discipline, as defined in EN 13292, and defines the regulatory aspects applicable to elements and processes for liquid, including cold gas, and electrical propulsion for spacecraft. It specifies the activities to perform in the engineering of such propulsion systems, their applicability, and defines the requirements for the engineering aspects: functional, configurational, interfaces, physical, environmental, quality factors, operational and verification.
General requirements relating to Mechanical Engineering are defined in EN 14607 Part 1.
This document applies only to liquid, including cold gas, and electrical propulsion systems used in spacecraft and to related mechanical parts. Solid propulsion for spacecraft, and solid and liquid propulsion for launchers are not covered by this document.
Other forms of propulsion currently under development (e.g. nuclear, nuclear-electric, solar-thermal and hybrid propulsion) are not presently covered by this document.
When viewed in 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.

Raumfahrttechnik - Mechanik - Teil 5-1: Antrieb

Ingénierie spatiale - Mécanique - Partie 5-1: Propulsion liquide et électrique pour satellites

Vesoljska tehnika – Mehanika – 5-1. del: Pogon za vesoljska plovila

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Withdrawn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
10-Sep-2014
Completion Date
28-Jan-2026

Relations

Effective Date
29-May-2013
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Standard

EN 14607-5-1:2005

English language
61 pages
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Frequently Asked Questions

EN 14607-5-1:2004 is a standard published by the European Committee for Standardization (CEN). Its full title is "Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft". This standard covers: EN 14607 Part 5.1 of Space engineering - Mechanical defined the requirements for the discipline liquid and electric propulsion for spacecraft This document belongs to the propulsion field of the mechanical discipline, as defined in EN 13292, and defines the regulatory aspects applicable to elements and processes for liquid, including cold gas, and electrical propulsion for spacecraft. It specifies the activities to perform in the engineering of such propulsion systems, their applicability, and defines the requirements for the engineering aspects: functional, configurational, interfaces, physical, environmental, quality factors, operational and verification. General requirements relating to Mechanical Engineering are defined in EN 14607 Part 1. This document applies only to liquid, including cold gas, and electrical propulsion systems used in spacecraft and to related mechanical parts. Solid propulsion for spacecraft, and solid and liquid propulsion for launchers are not covered by this document. Other forms of propulsion currently under development (e.g. nuclear, nuclear-electric, solar-thermal and hybrid propulsion) are not presently covered by this document. When viewed in 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.

EN 14607 Part 5.1 of Space engineering - Mechanical defined the requirements for the discipline liquid and electric propulsion for spacecraft This document belongs to the propulsion field of the mechanical discipline, as defined in EN 13292, and defines the regulatory aspects applicable to elements and processes for liquid, including cold gas, and electrical propulsion for spacecraft. It specifies the activities to perform in the engineering of such propulsion systems, their applicability, and defines the requirements for the engineering aspects: functional, configurational, interfaces, physical, environmental, quality factors, operational and verification. General requirements relating to Mechanical Engineering are defined in EN 14607 Part 1. This document applies only to liquid, including cold gas, and electrical propulsion systems used in spacecraft and to related mechanical parts. Solid propulsion for spacecraft, and solid and liquid propulsion for launchers are not covered by this document. Other forms of propulsion currently under development (e.g. nuclear, nuclear-electric, solar-thermal and hybrid propulsion) are not presently covered by this document. When viewed in 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.

EN 14607-5-1:2004 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 14607-5-1:2004 has the following relationships with other standards: It is inter standard links to EN 16603-35-01:2014, EN 14101:2001, EN 13701:2001, EN 14725:2003, EN 13292:1999. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 14607-5-1:2004 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 14607-5-1:2004 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 – 5-1. del: Pogon za vesoljska plovilaRaumfahrttechnik - Mechanik - Teil 5-1: AntriebIngénierie spatiale - Mécanique - Partie 5-1: Propulsion liquide et électrique pour satellitesSpace engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 14607-5-1:2004SIST EN 14607-5-1:2005en01-januar-2005SIST EN 14607-5-1:2005SLOVENSKI
STANDARD
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