Abstract

This Standard specifies: • Requirements for the following crimping wire connections intended for high reliability electrical connections for use on spacecraft and associated equipment operating under high vacuum, thermal cycling and launch vibration:  removable contacts, single wire  removable contacts, multiple wires  coaxial contacts, ferrules  lugs and splices.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	British Standards Institution
ProductNote	THIS STANDARD ALSO REFERS TO EN 16602-70-38
Pages
ISBN
Committee	ACE/68
Supersedes	BS EN 16602-70-26 : 2014