AMS-5904 / 5911, ASTM-A-666

Physical Properties
  • Minimum Tensile Strength - 150 ksi
  • Minimum Yield Strength (0.2% Offset) - 110 ksi
  • Elongation in 2 Inches (0.005 to 0.0150" Thick) - 9%
  • Elongation in 2 Inches (Over 0.0150" Thick) - 10%
  • Maximum Hardness - 32 HRC (Product shall not be rejected on the basis of hardness if tensile properties … are acceptable)
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Unit of Measure
Items
0.0310 Inch (in) Thickness Stainless Steel Sheets

T302 / 304 Half Hard 0.0310" x 12" x 12"
List Price $105.00
0.0310 Inch (in) Thickness Stainless Steel Sheets

T302 / 304 Half Hard 0.0310" x 12" x 18"
List Price $115.00
0.0310 Inch (in) Thickness Stainless Steel Sheets

T302 / 304 Half Hard 0.0310" x 12" x 24"
List Price $125.00
0.0310 Inch (in) Thickness Stainless Steel Sheets

T302 / 304 Half Hard 0.0310" x 24" x 24"
List Price $145.00
0.0310 Inch (in) Thickness Stainless Steel Sheets

T302 / 304 Half Hard 0.0310" x 24" x 36"
List Price $165.00
Description N/A AMS-5904 / 5911, ASTM-A-666

Physical Properties
  • Minimum Tensile Strength - 150 ksi
  • Minimum Yield Strength (0.2% Offset) - 110 ksi
  • Elongation in 2 Inches (0.005 to 0.0150" Thick) - 9%
  • Elongation in 2 Inches (Over 0.0150" Thick) - 10%
  • Maximum Hardness - 32 HRC (Product shall not be rejected on the basis of hardness if tensile properties … are acceptable)
Width N/A 12 in N/A 12 in N/A 12 in N/A 24 in N/A 24 in
Length N/A 12 in N/A 18 in N/A 24 in N/A 24 in N/A 36 in
Alloy N/A T302 / 304 Stainless Steel Alloy
Thickness N/A 0.0310 in
Thickness Tolerance N/A 0.001 in
American Society for Testing and Materials (ASTM) Steel Standard N/A ASTM-A-666
Aerospace Material Specification (AMS) N/A AMS-5904 / 5911
Alloy Steel Type N/A Stainless Steel
Material Form N/A Sheet
Temper N/A Half Hard 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 10.00 %
Maximum Molybdenum Composition N/A 0.75 %
Maximum Copper Composition N/A 0.75 %
Chemical Composition Table N/A

Minimum Tensile Strength N/A 150 ksi
Minimum Yield Strength (0.2 Percent (%) Offset) N/A 110 ksi
Minimum Elongation in 2 Inch (in) (0.005 to 0.0150 Inch (in) Thick) N/A 9 %
Minimum Elongation in 2 Inch (in) (Over 0.0150 Inch (in) Thick) N/A 10 %
Minimum Hardness1 N/A 32 Rockwell C
  • 1 Product shall not be rejected on the basis of hardness if tensile properties are acceptable