This Standard has been cancelled and replaced by ECSS-Q-ST-70-26C Rev.1 Corrigendum 1 (1 June 2017).
Scope
This Standard specifies:
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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:
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removable contacts, single wires
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removable contacts, multiple wires
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coaxial connectors, ferrules
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lugs and splices.
NOTE These are the most common used crimping wire termination and are represented in Figure 1
Attachments:
Md5 checksum .doc file = 05BB3981BCE037E1E206ECE1592848D4
Md5 checksum .pdf file = 1F8BC627A829AE880BA71725F505D39D
This standard cancels and replaces ECSS-Q-70-26A (13 February 2001).