EN 14607-2:2004
(Main)Space engineering - Mechanical - Part 2: Structural
Space engineering - Mechanical - Part 2: Structural
Part 2 of Space engineering - Mechanical defines the mechanical engineering requirements for structural engineering.
This document specifies the requirements to consider in all engineering aspects of structures: requirement definition and specification, design, development, verification, production, inservice and eventual disposal.
The document applies to all general structural subsystem aspects of space including: launch vehicles, transfer vehicles, reentry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems.
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.
Raumfahrttechnik - Mechanik - Teil 2: Strukturen
Ingénierie spatiale - Mécanique - Partie 2: Structure
Vesoljska tehnika – Mehanika – 2. del: Konstrukcija
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- Withdrawn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
- 13-Aug-2014
- Completion Date
- 21-Jan-2026
Relations
- Effective Date
- 29-May-2013
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Frequently Asked Questions
EN 14607-2:2004 is a standard published by the European Committee for Standardization (CEN). Its full title is "Space engineering - Mechanical - Part 2: Structural". This standard covers: Part 2 of Space engineering - Mechanical defines the mechanical engineering requirements for structural engineering. This document specifies the requirements to consider in all engineering aspects of structures: requirement definition and specification, design, development, verification, production, inservice and eventual disposal. The document applies to all general structural subsystem aspects of space including: launch vehicles, transfer vehicles, reentry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems. 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.
Part 2 of Space engineering - Mechanical defines the mechanical engineering requirements for structural engineering. This document specifies the requirements to consider in all engineering aspects of structures: requirement definition and specification, design, development, verification, production, inservice and eventual disposal. The document applies to all general structural subsystem aspects of space including: launch vehicles, transfer vehicles, reentry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems. 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.
EN 14607-2:2004 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 14607-2:2004 has the following relationships with other standards: It is inter standard links to EN 16603-32:2014. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 14607-2:2004 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 14607-2:2004 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 – 2. del: KonstrukcijaRaumfahrttechnik - Mechanik - Teil 2: StrukturenIngénierie spatiale - Mécanique - Partie 2: StructureSpace engineering - Mechanical - Part 2: Structural49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 14607-2:2004SIST EN 14607-2:2005en01-januar-2005SIST EN 14607-2:2005SLOVENSKI
STANDARD
SIST EN 14607-2:200
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