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AMS-5510, ASTM-A-240

Physical Properties
  • Minimum Tensile Strength (0.002 to 0.003" Thick) - 70 to 110 ksi
  • Minimum Tensile Strength (0.003 to 0.004" Thick) - 70 to 105 ksi
  • Minimum Tensile Strength (Over 0.004" Thick) - 70 to 100 ksi
  • Minimum Yield Strength (0.2% Offset) - 25.0 ksi
  • Elongation in 2 Inches (0.002 to 0.003" Thick) - 20%
  • Elongation in 2 Inches (0.003 to 0.004" Thick) - 30%
  • Elongation in 2 Inches (Over 0.004" Thick) - 40%
  • Minimum Hardness - No Req.
Unit of Measure

Specifications

Width

12 in

Length

24 in

Alloy

T321 Stainless Steel Alloy

Thickness

0.0100 in

Thickness Tolerance

5 %

American Society for Testing and Materials (ASTM) Steel Standard

ASTM-A-240

Aerospace Material Specification (AMS)

AMS-5510

Alloy Steel Type

Stainless Steel

Material Form

Sheet

Temper

Annealed Temper

Chemical Composition

Maximum Carbon Composition

0.08 %

Maximum Manganese Composition

2.00 %

Maximum Silicon Composition

1.00 %

Maximum Phosphorus Composition

0.04 %

Maximum Sulfur Composition

0.03 %

Maximum Chromium Composition

19.00 %

Maximum Nickel Composition

12.00 %

Maximum Titanium Composition

0.70 %

Maximum Molybdenum Composition

0.75 %

Maximum Copper Composition

0.75 %

Maximum Nitrogen Composition

0.10 %

Chemical Composition Table



Physical Properties

Minimum Tensile Strength (0.002 to 0.003 Inch (in) Thick)

70 to 110 ksi

Minimum Tensile Strength (0.003 to 0.004 Inch (in) Thick)

70 to 105 ksi

Minimum Tensile Strength (Over 0.004 Inch (in) Thick)

70 to 100 ksi

Minimum Yield Strength (0.2 Percent (%) Offset)

25.0 ksi

Minimum Elongation in 2 Inch (in) (0.002 to 0.003 Inch (in) Thick)

20 %

Minimum Elongation in 2 Inch (in) (0.003 to 0.004 Inch (in) Thick)

30 %

Minimum Elongation in 2 Inch (in) (Over 0.004 Inch (in) Thick)

40 %