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
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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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