EN 14607-2:2004

Space engineering - Mechanical - Part 2: Structural EN 14607-2:2004

Publication date:   Dec 28, 2004

General information

99.60   Withdrawal effective   Aug 13, 2014

CEN

CEN/BT

European Norm

49.140   Space systems and operations

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Scope

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.

Life cycle

NOW

WITHDRAWN
EN 14607-2:2004
99.60 Withdrawal effective
Aug 13, 2014

REVISED BY

PUBLISHED
EN 16603-32:2014

Relations

Adopted from ECSS-E-30-2 IDENTICAL




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