SAE ARP1481A
Superseded
View Superseded by
Corrosion Control and Electrical Conductivity in Enclosure Design
Hardcopy , PDF
English
08-18-2004
02-29-2024
1 SCOPE
2 REFERENCES
3 BACKGROUND
Sets up a compatibility table having as its objective a listing of metallic couples compatible from a corrosion aspect and which still maintain a low contact impedance.
| DocumentType |
Standard
|
| Pages |
5
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
Corrosion control is always of concern to the designer of electronic enclosures. The use of EMI gaskets to provide shielding often creates requirements that are in conflict with ideal corrosion control. This SAE Aerospace Recommended Practice (ARP) presents a compatibility table (see Figure 1) which has as its objective a listing of metallic couples that are compatible from a corrosion aspect and which still maintain a low contact impedance.
| NASA-STD-6012A:2022 | CORROSION PROTECTION FOR SPACE FLIGHT HARDWARE |
| MIL-M-3171 Revision C:1966 | Magnesium Alloy, Processes for Pretreatment and Prevention of Corrosion on (S/S by SAE-AMS-M-3171) |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : All end users must be registered with an Account prior to user licenses being assigned.
Users cannot be edited or removed once added to your Multi user PDF.