Standards Worldwide
Standards Worldwide
Phone +49 30 58885700-07

Standard [CURRENT]

DIN EN 16602-70-36:2015-06

Space product assurance - Material selection for controlling stress-corrosion cracking; English version EN 16602-70-36:2014

German title
Raumfahrtproduktsicherung - Kriterien für die Werkstoffwahl zur Vermeidung von Spannungsrisskorrosion; Englische Fassung EN 16602-70-36:2014
Publication date
2015-06
Original language
English
Pages
43

Please select

from 117.70 EUR VAT included

from 110.00 EUR VAT excluded

Purchasing options

PDF download
  • 117.70 EUR

Shipment (3-5 working days)
  • 142.60 EUR

Standards Ticker 1
1

Learn more about the standards ticker

Publication date
2015-06
Original language
English
Pages
43
DOI
https://dx.doi.org/10.31030/2311026

Quick delivery via download or delivery service

Buy securely with a credit card or pay upon receipt of invoice

All transactions are encrypted

Overview

This standard covers the following processes of the general materials, mechanicals parts and processes (MMPP) flow of ECSS-Q-ST-70: The selection of metal alloys for which preference is given to approved data sources (Table 5-1 to Table 5-3). The criticality analysis to determine if a stress corrosion cracking (SCC) evaluation is necessary. This standard sets forth the criteria to be used in the selection of materials for spacecraft and associated equipment and facilities so that failure resulting from stress-corrosion is prevented. It is intended to provide general criteria to be used in stress-corrosion cracking control, which begins during design thanks to a methodological material selection. This document does not intend to include all factors and criteria necessary for the total control of stress corrosion cracking in all alloys. The criteria established in this standard are only applicable to designs for service involving exposure conditions similar to testing conditions As regards weldments, this standard is applicable to aluminium alloys, selected stainless steels in the 300 series and alloys listed in Table 5-1. This standard is not applicable to listed materials whose behaviour differs at elevated temperature and in specific chemical. 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 16602-70-36:2014) has been prepared by Technical Committee CEN/CLC/TC 5 "Space", the secretariat of which is held by DIN (Germany). This document supersedes DIN EN 14101:2002-10. 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).

Content
ICS
49.025.01, 49.140
DOI
https://dx.doi.org/10.31030/2311026
Replacement amendments

This document replaces DIN EN 14101:2002-10 .

Cooperation at DIN

Loading recommended items...
Loading recommended items...
Loading recommended items...