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Normas BSI – AENOR
BS EN 16603-32-01:2014

BS EN 16603-32-01:2014

Space engineering. Fracture control

Fecha:
2014-08-31 /Revision Underway
Comité:
ACE/68
Equivalencias internacionales:

EN 16603-32-01:2014

Relación con otras normas BSI:

Reemplaza a: BS EN 14165:2004

Resumen:
This ECSS Engineering Standard specifies the fracture control requirements to be imposed on space segments of space systems and their related GSE. The fracture control programme is applicable for space systems and related GSE when required by ECSS-Q-ST-40 or by the NASA document NST 1700.7, incl. ISS addendum. The requirements contained in this Standard, when implemented, also satisfy the fracture control requirements applicable to the NASA STS and ISS as specified in the NASA document NSTS 1700.7 (incl. the ISS Addendum). The NASA nomenclature differs in some cases from that used by ECSS. When STS/ISS-specific requirements and nomenclature are included, they are identified as such. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Keywords:
Inspection, Fracture, Quality assurance, Air transport engineering, Defects, Space technology, Fatigue testing, Cracking, Tensile testing, Plane strain fracture toughness tests
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