SS-EN-16602-70-26 › Space product assurance - Crimping of high-reliability electrical connections
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This Standard specifies: Requirements for the following crimping wire terminations intended for high reliability electrical connections for use on customer spacecraft and associated equipment operating under high vacuum, thermal cycling and launch vibration: removable contacts, single wires removable contacts, multiple wires coaxial connectors, ferrules lugs and splices. NOTE These are the most common used crimping wire termination and are represented in Figure 1 1. The general conditions to be met for the approval of terminations other than the above mentioned ones. NOTE Additional forms of crimps, not covered in this standard, are listed (not exhaustively) in the informative Annex A. Product assurance provisions for both the specific and the generic terminations mentioned above. Training and certification requirements for operators and inspectors (clause 5.5.2), additional to those specified in ECSS Q ST-20. This standard may be tailored for the specific characteristics and constraints of a space project, in conformance with ECSS-S-ST-00.
To find similar documents by classification:
49.060 (Aerospace electric equipment and systems Including Avionics)
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Designation Name
SS-EN 16602-70-26:2019
Revision Level
2019 EDITION
Status
Current
Publication Date
March 20, 2019
Language(s)
English
Page Count
64
International Equivalent
EN 16602-70-26:2019(IDT)