Standard [CURRENT]
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This standard specifies requirements for mechanical testing of metallic materials to be used in the fabrication of spacecraft hardware. This standard establishes the requirements for most relevant test methods carried out to assess the tensile, fatigue and fracture properties of metallic materials. It does not give a complete review of all the existing test methods for the evaluation of mechanical properties of metallic materials. Furthermore, this standard specifies requirements for the evaluation, presentation and reporting of test results. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00. This document (DIN EN 16602-70-37:2014) has been prepared by Technical Committee CEN/CLC/TC 5 "Space", the secretariat of which is held by DIN (Germany). This document has been developed to cover specifically space systems and has therefore precedence over any EN covering the same scope but with a wider domain of applicability (for example: aerospace). The responsible German body involved in its preparation is Working Committee NA 131-10-01 AA "Interoperabilität von Informations-, Kommunikations- und Navigationssystemen" ("Interoperability of information, communication and navigation systems") at the DIN Standards Committee Aerospace (NL).