- 5052
- UNS A 95052
- NON-HEAT TREATABLE
Magnesium gives this alloy its enhanced corrosion resistance, workability, strength, and weldability. Typical uses include aircraft fuel tanks, electronic mounting plates and panels, fan blades, refrigeration liners, storm shutters, and utensils.
| Chemical Composition Limits (%) |
| SiliconSi |
IronFe |
CopperCu |
ManganeseMn |
MagnesiumMg |
ChromiumCr |
NickelNi |
ZincZn |
TitaniumTi |
OthersEach |
Total |
AluminumMin |
| 0.25 |
0.4 |
0.10 |
0.10 |
2.2-2.8 |
0.15-0.35 |
|
0.10 |
|
0.05 |
0.15 |
Remainder |
Weldability and resistance to corrosion is considered favorable. This type of alloy is used for body panel sheet because its formability is very good. Resistance to corrosion is good except when material is held at elevated temperatures for long periods of time.
| Chemical Composition Limits (%) |
| SiliconSi |
IronFe |
CopperCu |
ManganeseMn |
MagnesiumMg |
ChromiumCr |
NickelNi |
ZincZn |
TitaniumTi |
OthersEach |
Total |
AluminumMin |
| 0.2 |
0.35 |
0.15 |
0.2-0.5 |
4.0-5.0 |
0.10 |
|
0.25 |
0.10 |
0.05 |
0.15 |
Remainder |
| Mechanical Property Limits |
View : |
| Alloy and Temper |
Specified Tickness |
Tensil Strength - KSI |
Elongation in 2 inches % |
| Ultimate |
Yield |
| Inches |
Min |
Max |
Min |
Max |
| 5052-0 |
0.006-0.007 |
25.0 |
31.0 |
9.5 |
- |
- |
| |
0.008-0.012 |
25.0 |
31.0 |
9.5 |
- |
14 |
| |
0.013-0.019 |
25.0 |
31.0 |
9.5 |
- |
15 |
| |
0.020-0.031 |
25.0 |
31.0 |
9.5 |
- |
16 |
| |
0.032-0.050 |
25.0 |
31.0 |
9.5 |
- |
18 |
| |
0.051-0.113 |
25.0 |
31.0 |
9.5 |
- |
19 |
| |
0.114-0.249 |
25.0 |
31.0 |
9.5 |
- |
20 |
| |
0.250-3.000 |
25.0 |
31.0 |
9.5 |
- |
18 |
| 5052-H32 |
0.017-0.019 |
31.0 |
38.0 |
23.0 |
- |
4 |
| |
0.020-0.050 |
31.0 |
38.0 |
23.0 |
- |
5 |
| |
0.051-0.113 |
31.0 |
38.0 |
23.0 |
- |
7 |
| |
0.114-0.249 |
31.0 |
38.0 |
23.0 |
- |
9 |
| |
0.250-0.499 |
31.0 |
38.0 |
23.0 |
- |
11 |
| |
0.500-2.000 |
31.0 |
38.0 |
23.0 |
- |
12 |
| 5052-H34 |
0.009-0.019 |
34.0 |
41.0 |
26.0 |
- |
3 |
| |
0.020-0.050 |
34.0 |
41.0 |
26.0 |
- |
4 |
| |
0.051-0.113 |
34.0 |
41.0 |
26.0 |
- |
6 |
| |
0.114-0.249 |
34.0 |
41.0 |
26.0 |
- |
7 |
| |
0.250-1.000 |
34.0 |
41.0 |
26.0 |
- |
10 |
| 5052-H36 |
0.006-0.007 |
37.0 |
44.0 |
29.0 |
- |
2 |
| |
0.008-0.031 |
37.0 |
44.0 |
29.0 |
- |
3 |
| |
0.032-0.162 |
37.0 |
44.0 |
29.0 |
- |
4 |
| 5052-H38 |
0.006-0.007 |
39.0 |
- |
32.0 |
- |
2 |
| |
0.008-0.031 |
39.0 |
- |
32.0 |
- |
3 |
| |
0.032-0.128 |
39.0 |
- |
32.0 |
- |
4 |
| 5052-H39 |
0.006-0.063 |
41.0 |
- |
- |
- |
1 |
| 5052-H112 |
0.250-0.499 |
28.0 |
- |
16.0 |
- |
7 |
| |
0.500-2.000 |
25.0 |
- |
9.5 |
- |
12 |
| |
2.001-3.000 |
25.0 |
- |
9.5 |
- |
16 |
| 5052-H391 |
0.008-0.125 |
42.0 |
- |
35.0 |
- |
3 |
- Chemical composition is percent maximum unless shown as a range or a minimum.
- Source: Aluminum Standards and Data-The Aluminum Association, Inc.
- Information presented as a guide for reference purposes only and is not intended to be used for product design or application.