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Normas DIN – AENOR
DIN EN 14165:2005-02

DIN EN 14165:2005-02

Space engineering standards - Fracture control; German version EN 14165:2004

Ingénierie Spatiale - Maîtrise de la rupture; Version allemande EN 14165:2004

Raumfahrttechnik - Überwachung des Rissfortschritts; Deutsche Fassung EN 14165:2004

Fecha Anulación:
2014-10 /Withdrawn
Equivalencias internacionales:

EN 14165 (2004-04)

Relación con otras normas DIN:

Reemplaza a: DIN EN 14165:2004-03

Reemplazada por: DIN EN 16603-32-01:2014-10

Resumen:
This standard specifies the fracture control requirements to be imposed on space systems. The requirements contained in this standard, when implemented, also satisfy the requirements applicable to the NASA STS and ISS as defined in the NASA document NSTS 1700.7 (incl. the ISS Addendum). Since this standard and the NASA document NSTS 1700.7 (incl. the ISS Addendum) are subject to different independent approval authorities, and recognizing that possible changes to documents may occur in the future, the user of this standard is advised to confirm the current status. NOTE The definitions used in this standard are based on ECSS nomenclature and are given in clause 3. The NASA nomenclature differs in some cases from that used by ECSS. When STS-specific requirements and nomenclature are included, they are identified as such.
Keywords:
Aerospace transport, Crack susceptibility, Crack tests, Cracking, Damage, Defects, Definitions, Evaluations, Flaws, Fracture state, Hazards, Inspection, Life (durability), Metalworking, Quality assurance, Resistance to crack formation, Space safety, Space transport, Specification (approval), Surveillance (approval), Testing, Testing conditions
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