SS-EN 16602-70-26 : 2019
Current
The latest, up-to-date edition.
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Hardcopy
English
27-03-2019
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.
| Committee |
TC 5
|
| DocumentType |
Standard
|
| Pages |
0
|
| PublisherName |
Standardiserings-Kommissionen I Sverige
|
| Status |
Current
|
| Standards | Relationship |
| EN 16602-70-26:2019 | Identical |
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