Width |
N/A 12 in |
Length |
N/A 24 in |
Alloy |
N/A T321 Stainless Steel Alloy |
Thickness |
N/A 0.0100 in |
Thickness Tolerance |
N/A 5 % |
American Society for Testing and Materials (ASTM) Steel Standard |
N/A ASTM-A-240 |
Aerospace Material Specification (AMS) |
N/A AMS-5510 |
Alloy Steel Type |
N/A Stainless Steel |
Material Form |
N/A Sheet |
Temper |
N/A Annealed Temper |
Maximum Carbon Composition |
N/A 0.08 % |
Maximum Manganese Composition |
N/A 2.00 % |
Maximum Silicon Composition |
N/A 1.00 % |
Maximum Phosphorus Composition |
N/A 0.04 % |
Maximum Sulfur Composition |
N/A 0.03 % |
Maximum Chromium Composition |
N/A 19.00 % |
Maximum Nickel Composition |
N/A 12.00 % |
Maximum Titanium Composition |
N/A 0.70 % |
Maximum Molybdenum Composition |
N/A 0.75 % |
Maximum Copper Composition |
N/A 0.75 % |
Maximum Nitrogen Composition |
N/A 0.10 % |
Chemical Composition Table |
N/A
|
Minimum Tensile Strength (0.002 to 0.003 Inch (in) Thick) |
N/A 70 to 110 ksi |
Minimum Tensile Strength (0.003 to 0.004 Inch (in) Thick) |
N/A 70 to 105 ksi |
Minimum Tensile Strength (Over 0.004 Inch (in) Thick) |
N/A 70 to 100 ksi |
Minimum Yield Strength (0.2 Percent (%) Offset) |
N/A 25.0 ksi |
Minimum Elongation in 2 Inch (in) (0.002 to 0.003 Inch (in) Thick) |
N/A 20 % |
Minimum Elongation in 2 Inch (in) (0.003 to 0.004 Inch (in) Thick) |
N/A 30 % |
Minimum Elongation in 2 Inch (in) (Over 0.004 Inch (in) Thick) |
N/A 40 % |