This Standard has been cancelled and replaced by ECSS-Q-ST-70-26C Rev.1 Corrigendum 1 (1 June 2017).
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
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This standard cancels and replaces ECSS-Q-70-26A (13 February 2001).