Stainless steel 301 301 (UNS S30100)
Fe balance, Cr 16.0 to 18.0, Ni 6.0 to 8.0, max 0.15 C, max 2.00 Mn, max 1.00 Si, max 0.045 P, max 0.030 S, max 0.10 N (wt%)
Also known as UNS S30100, EN 1.4310, AISI 301, JIS SUS 301, BS 301S21, AFNOR Z11 CN 18-08 · 10 more
Type 301 is a chromium-nickel austenitic stainless steel, nominally 17 percent chromium and 7 percent nickel (ATI).
Evidence level
2 of 5
Lab-measured
- 0Predicted only. No one has made it, or no measurement exists.
- 1Calculated. Only calculated or predicted values from sources.
- 2Lab-measured. Measured properties with their conditions stated.
- 3Space-relevant tests. Measured in conditions relevant to space, such as vacuum or atomic oxygen.
- 4Ground-qualified. Qualified for an application on the ground.
- 5Flown or field-proven. Flight or field results exist.
Strength by temper
515 MPa
Yield by temper
205 MPa
How fast it work hardens
0.8 -
Stiffness
193 GPa
Heat
552 MPa at 204 C
Recipe, share of the weight
- Fe balance (the rest)Iron
- Cr 16 to 18%Chromium
- Ni 6 to 8%Nickel
- Mn 0 to 2%Manganese
- Si 0 to 1%Silicon
- C 0 to 0.15%Carbon
- N 0 to 0.1%Nitrogen
- P 0 to 0.045%Phosphorus
- S 0 to 0.03%Sulfur
Best for
Springs, clips and light formed structures where cold-work strength matters more than corrosion resistance
Weakest at
Chloride pitting (critical pitting temperature below 10 C in Outokumpu's test) and carbide precipitation after welding or holding at 427 to 816 C
Risk at a glance
- People Low. Fume and skin contact are the hazards
- If it fails High. Grain-boundary carbide precipitation after welding or holding
- Corrosion Moderate. Critical pitting temperature below 10 C in Outokumpu's potentiostatic test.
Quick facts: 301 (UNS S30100)
| Property | Value | Basis |
|---|---|---|
| Density | 7.88 to 8.03 g/cm³ | 3 sourced values across conditions |
| Yield strength | 205 to 1,103 MPa | 10 sourced values across conditions |
| Tensile strength | 515 to 1,276 MPa | 5 sourced values across conditions |
| Young's modulus | 174 to 200 GPa | 4 sourced values across conditions |
| Thermal conductivity | 16.3 to 21.4 W/(m·K) | 2 sourced values across conditions |
| Thermal expansion (CTE) | 16.6 to 19.8 ppm/K | 3 sourced values across conditions |
| Melting point | 1,399 to 1,421 °C | 1 sourced value |
| Specific heat | 500 J/(kg·K) | 1 sourced value |
| Electrical resistivity | 7.2e-7 Ω·m | 1 sourced value |
| Maximum service temperature | 840 °C | 1 sourced value |
What is the density of Stainless steel 301?
Stainless steel 301 has a density of 7.88 to 8.03 g/cm³. The range covers 3 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What is the thermal conductivity of Stainless steel 301?
Stainless steel 301 has a thermal conductivity of 16.3 to 21.4 W/(m·K). The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What is the coefficient of thermal expansion of Stainless steel 301?
Stainless steel 301 has a coefficient of thermal expansion of 16.6 to 19.8 ppm/K. The range covers 3 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What is the melting point of Stainless steel 301?
Stainless steel 301 has a melting point of 1,399 to 1,421 °C. The source and test conditions are listed in the properties table on this page.
What is the yield strength of Stainless steel 301?
Stainless steel 301 has a yield strength of 205 to 1,103 MPa. The range covers 10 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.
What are the other names and codes for Stainless steel 301?
Stainless steel 301 is also written as UNS S30100, EN 1.4310, AISI 301, JIS SUS 301, BS 301S21, AFNOR Z11 CN 18-08. Each code is printed in the source listed beside it in the designations table.
What is Stainless steel 301 used for?
Uses recorded in the sources include Aircraft structural parts; Truck and trailer bodies, railway and subway cars; Springs and hose clamps.
Why it exists
Type 301 is the cold-work grade of the stainless family. ATI says its tensile strength in the work-hardened condition is higher than other stable austenitic grades, and ATI and UPMET list springs, aircraft structural parts, truck and trailer bodies and railway cars as uses. Its limits are corrosion resistance below the 18-8 grades and carbide precipitation on welding.
Where it's used
Aircraft structural parts
UPMET lists aircraft structural parts among the industry applications for its 301 sheet and coil. It also lists trailer bodies, architectural parts and conveyor parts.
Truck and trailer bodies, railway and subway cars
ATI names truck and trailer bodies and railway and subway cars among the major applications for 301.
Springs
ATI names springs and hose clamps among the major applications for 301, alongside automobile trim and kitchen equipment.
Recipe
Fe balance, Cr 16.0 to 18.0, Ni 6.0 to 8.0, max 0.15 C, max 2.00 Mn, max 1.00 Si, max 0.045 P, max 0.030 S, max 0.10 N (wt%)
Type 301 is an iron-based austenitic stainless steel. ATI and UPMET give the same composition limits: 16 to 18 percent chromium and 6 to 8 percent nickel, with maximum limits on carbon, manganese, silicon, phosphorus, sulfur and nitrogen, and iron as the balance. It is sold as cold-rolled strip, sheet and plate, and its temper, from annealed to full hard, is set by how much it is cold rolled (ATI).
| Ingredient | Share of the weight | What it does |
|---|---|---|
| Iron Fe | balance (the rest) | The matrix of the alloy. It holds the austenite structure that gives 301 its ductility. |
| Chromium Cr | 16 to 18% | Forms the passive oxide film that gives corrosion resistance. |
| Nickel Ni | 6 to 8% | Holds the austenite structure at room temperature. |
| Manganese Mn | 0 to 2% | Deoxidiser in the melt; the printed limit is a maximum. |
| Silicon Si | 0 to 1% | Deoxidiser in the melt; the printed limit is a maximum. |
| Carbon C | 0 to 0.15% | Adds strength, but chromium carbide can form at the grain boundaries when the steel is held between 427 and 816 C (ATI). |
| Nitrogen N | 0 to 0.1% | Held to a maximum; it adds strength in austenite. |
| Phosphorus P | 0 to 0.045% | Impurity held low. |
| Sulfur S | 0 to 0.03% | Impurity held low. |
Weight shares are as printed in the sources.
What it can do
Strength by temper
515 MPa
measured
Minimum tensile strength is 515 MPa annealed, 862 MPa quarter hard, 1034 MPa half hard, 1207 MPa three-quarter hard and 1276 MPa full hard (ASTM A240 and A666 minimums, ATI).
Yield by temper
205 MPa
measured
Minimum yield strength is 205 MPa annealed and 965 MPa full hard (ATI). The three-quarter hard minimum is 931 MPa.
How fast it work hardens
0.8 -
measured
Typical as-rolled yield rises from 248 MPa annealed to 552 MPa quarter hard and 1103 MPa full hard (ATI). Outokumpu prints a strain-hardening exponent of 0.8 for 1.4310, the highest value in its forming column.
Stiffness
193 GPa
measured
Elastic modulus is 193 GPa for annealed material (ATI) and falls to 174 GPa for full-hard material as rolled (ATI).
Heat
552 MPa at 204 C
measured
Annealed material keeps a typical tensile strength of 552 MPa at 204 C and 401 MPa at 538 C (ATI).
Cold
2082 MPa at -196 C, full hard
measured
At -196 C full-hard material has a typical tensile strength of 2082 MPa and a yield of 1482 MPa (ATI). The annealed material reaches 1896 MPa at the same temperature.
How it compares
Compared with the 18-8 grades, ATI says 301's corrosion properties are not as good, and carbide precipitation during welding restricts its use in favour of ATI 304 and 304L. Once work hardened, ATI says 301 develops higher tensile strength than other stable austenitic grades. Outokumpu's strain-hardening exponent of 0.8 is the highest in its forming column.
The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details. Other materials are shown beside it; each was measured under its own conditions, so open its page before comparing closely. Compare every grade in the family.
| Measurement | 301 (UNS S30100) | 304 (UNS S30400) | 303 (UNS S30300) | 316 (UNS S31600) | 316L (UNS S31603) | 302 | 304L (UNS S30403) | 309 | 310S (UNS S31008, EN 1.4845) | 317L | 321 | 347 | 347H | 904L (UNS N08904, EN 1.4539) | Nitronic 60 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Thermal behavior and safety | |||||||||||||||
| melting point | 1399 to 1421 °C4 | 1673 K | 1455 °C | 1390 °C | 1390 °C | 1420 °C | 1399 to 1421 °C | 2550 to 2650 °F | 1410 °C | 1390 to 1440 °C | 1398 to 1446 °C | 1398 to 1446 °C | 2550 to 2635 degF | 1300 to 1390 °C | no data |
| Thermal conductivity | 16.3 W/m.K7 | 14 W/m.K | 15 W/m°C | 14.6 W/m.K | 14.6 W/m·K | 16.2 W/(m·K) | 16.3 W/m·K | 15.6 W/m·K | 13 W/(m·K) | 14 W/(m·K) | 16.3 W/(m·K) | 16.3 W/(m·K) | 14 W/m.°C | 12 W/(m·K) | 9 Btu/ft hr °F |
| Thermal conductivity | 21.4 W/m.K8 | 14 W/m.K | 15 W/m°C | 14.6 W/m.K | 14.6 W/m·K | 16.2 W/(m·K) | 16.3 W/m·K | 15.6 W/m·K | 13 W/(m·K) | 14 W/(m·K) | 16.3 W/(m·K) | 16.3 W/(m·K) | 14 W/m.°C | 12 W/(m·K) | 9 Btu/ft hr °F |
| specific heat | 500 J/kg.K9 | 490 J/kg.K | 500 J/kg°C | 450 J/kg.K | 450 J/kg °K | 500 J/kg K | 500 J/kg·K | 502 J/kg·K | 480 J/(kg·K) | 500 J/(kg·K) | 500 J/kg K | 500 J/(kg·K) | 485 J/(kg.°C) | 450 J/(kg·K) | 0.12 Btu/lb °F |
| Physical and electrical | |||||||||||||||
| Density | 8.03 g/cm³1 | 7.85 Mg/m3 | 7.9 kg/dm3 | 8.027 g/cm³ | 8.03 g/cm³ | 7.9 g/cm³ | 7.9 g/cm³ | 8.03 g/cm³ | 7.8 kg/dm3 | 8.027 g/cm³ | 7.92 g/cm³ | 7.96 g/cm³ | 7.98 kg/dm3 | 7.95 g/cm³ | 7.622 gm/cm³ |
| Density | 7.88 g/cm³2 | 7.85 Mg/m3 | 7.9 kg/dm3 | 8.027 g/cm³ | 8.03 g/cm³ | 7.9 g/cm³ | 7.9 g/cm³ | 8.03 g/cm³ | 7.8 kg/dm3 | 8.027 g/cm³ | 7.92 g/cm³ | 7.96 g/cm³ | 7.98 kg/dm3 | 7.95 g/cm³ | 7.622 gm/cm³ |
| Density | 7.9 g/cm³3 | 7.85 Mg/m3 | 7.9 kg/dm3 | 8.027 g/cm³ | 8.03 g/cm³ | 7.9 g/cm³ | 7.9 g/cm³ | 8.03 g/cm³ | 7.8 kg/dm3 | 8.027 g/cm³ | 7.92 g/cm³ | 7.96 g/cm³ | 7.98 kg/dm3 | 7.95 g/cm³ | 7.622 gm/cm³ |
| electrical resistivity | 72 µΩ·cm13 | 65 10-8 ohm.m | 72 microhm-cm | 69 10-8 ohm.m | 74 μΩ·cm | 72 µΩ·cm | 72 microhm-cm | 78 µΩ·cm | 0.86 Ω·mm²/m | 475 Ohm-circ mil/ft | 72 microhm·cm | 72 µΩ·cm | no data | 95.2 µΩ·cm | 98.2 microhm-cm |
| electrical resistivity | 100 µΩ·cm14 | 65 10-8 ohm.m | 72 microhm-cm | 69 10-8 ohm.m | 74 μΩ·cm | 72 µΩ·cm | 72 microhm-cm | 78 µΩ·cm | 0.86 Ω·mm²/m | 475 Ohm-circ mil/ft | 72 microhm·cm | 72 µΩ·cm | no data | 95.2 µΩ·cm | 98.2 microhm-cm |
| hardness | 85 HRB38 | no data | < 202 HBN | < 217 HB | no data | no data | no data | no data | no data | no data | no data | < 201 HB | < 201 HB | < 230 HB | > 85 HRB |
| hardness | 25 HRC39 | no data | < 202 HBN | < 217 HB | no data | no data | no data | no data | no data | no data | no data | < 201 HB | < 201 HB | < 230 HB | > 85 HRB |
| hardness | 32 HRC40 | no data | < 202 HBN | < 217 HB | no data | no data | no data | no data | no data | no data | no data | < 201 HB | < 201 HB | < 230 HB | > 85 HRB |
| hardness | 37 HRC41 | no data | < 202 HBN | < 217 HB | no data | no data | no data | no data | no data | no data | no data | < 201 HB | < 201 HB | < 230 HB | > 85 HRB |
| hardness | 41 HRC42 | no data | < 202 HBN | < 217 HB | no data | no data | no data | no data | no data | no data | no data | < 201 HB | < 201 HB | < 230 HB | > 85 HRB |
| Other measurements | |||||||||||||||
| elastic modulus | 193 GPa5 | 200 GPa | 193 GPa | 200 GPa | 193 GPa | 200 GPa | 200 GPa | 200 GPa | 195 GPa | 200 GPa | 193 GPa | 193 GPa | 200 GPa | 195 GPa | 180 GPa |
| elastic modulus | 200 GPa6 | 200 GPa | 193 GPa | 200 GPa | 193 GPa | 200 GPa | 200 GPa | 200 GPa | 195 GPa | 200 GPa | 193 GPa | 193 GPa | 200 GPa | 195 GPa | 180 GPa |
| Thermal expansion (CTE) | 16.6 10-6/K10 | no data | 16 10-6/°C | 16.5 10-6/K | 16.5 10-6 cm/cm/°C | 16.6 µm/(m·°C) | 16.6 10-6 cm/cm/°C | 15.6 µm/(m·K) | 16.5 ppm/K | 16.5 10^-6 cm/cm/°C | 16.6 ppm/K | 16.6 ppm/K | 9.2 in/in.degF x 10^-6 | 15.8 ppm/K | 15.8 µm/m/°C |
| Thermal expansion (CTE) | 18.6 10-6/K11 | no data | 16 10-6/°C | 16.5 10-6/K | 16.5 10-6 cm/cm/°C | 16.6 µm/(m·°C) | 16.6 10-6 cm/cm/°C | 15.6 µm/(m·K) | 16.5 ppm/K | 16.5 10^-6 cm/cm/°C | 16.6 ppm/K | 16.6 ppm/K | 9.2 in/in.degF x 10^-6 | 15.8 ppm/K | 15.8 µm/m/°C |
| Thermal expansion (CTE) | 19.8 10-6/K12 | no data | 16 10-6/°C | 16.5 10-6/K | 16.5 10-6 cm/cm/°C | 16.6 µm/(m·°C) | 16.6 10-6 cm/cm/°C | 15.6 µm/(m·K) | 16.5 ppm/K | 16.5 10^-6 cm/cm/°C | 16.6 ppm/K | 16.6 ppm/K | 9.2 in/in.degF x 10^-6 | 15.8 ppm/K | 15.8 µm/m/°C |
| Oxidation resistance limit in air, as printed | 840 °C15 | no data | no data | 1023 K | no data | 925 °C | < 426 °C | 2000 °F | 1050 °C | no data | 850 °C | 800 °C | 850 °C | < 400 °C | no data |
| ultimate tensile strength | 515 MPa16 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| ultimate tensile strength | 862 MPa17 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| ultimate tensile strength | 1034 MPa18 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| ultimate tensile strength | 1207 MPa19 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| ultimate tensile strength | 1276 MPa20 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| yield strength | 205 MPa21 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 517 MPa22 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 758 MPa23 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 931 MPa24 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 965 MPa25 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| elongation | 40 %26 | > 40 % | > 35 % | 40 % | 40 % | 55 % | > 40 % | 49 % | 42 % | > 40 % | > 35 % | > 40 % | > 40 % | > 35 % | > 35 % |
| elongation | 25 %27 | > 40 % | > 35 % | 40 % | 40 % | 55 % | > 40 % | 49 % | 42 % | > 40 % | > 35 % | > 40 % | > 40 % | > 35 % | > 35 % |
| elongation | 18 %28 | > 40 % | > 35 % | 40 % | 40 % | 55 % | > 40 % | 49 % | 42 % | > 40 % | > 35 % | > 40 % | > 40 % | > 35 % | > 35 % |
| elongation | 12 %29 | > 40 % | > 35 % | 40 % | 40 % | 55 % | > 40 % | 49 % | 42 % | > 40 % | > 35 % | > 40 % | > 40 % | > 35 % | > 35 % |
| elongation | 9 %30 | > 40 % | > 35 % | 40 % | 40 % | 55 % | > 40 % | 49 % | 42 % | > 40 % | > 35 % | > 40 % | > 40 % | > 35 % | > 35 % |
| yield strength | 248 MPa31 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 552 MPa32 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 841 MPa33 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 979 MPa34 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| yield strength | 1103 MPa35 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| elastic modulus | 193 GPa36 | 200 GPa | 193 GPa | 200 GPa | 193 GPa | 200 GPa | 200 GPa | 200 GPa | 195 GPa | 200 GPa | 193 GPa | 193 GPa | 200 GPa | 195 GPa | 180 GPa |
| elastic modulus | 174 GPa37 | 200 GPa | 193 GPa | 200 GPa | 193 GPa | 200 GPa | 200 GPa | 200 GPa | 195 GPa | 200 GPa | 193 GPa | 193 GPa | 200 GPa | 195 GPa | 180 GPa |
| ultimate tensile strength | 552 MPa43 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| yield strength | 152 MPa44 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| ultimate tensile strength | 401 MPa45 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| yield strength | 126 MPa46 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| ultimate tensile strength | 1896 MPa47 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| yield strength | 517 MPa48 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| elongation | 30 %49 | > 40 % | > 35 % | 40 % | 40 % | 55 % | > 40 % | 49 % | 42 % | > 40 % | > 35 % | > 40 % | > 40 % | > 35 % | > 35 % |
| ultimate tensile strength | 2082 MPa50 | > 515 MPa | > 517 MPa | 515 MPa | 485 MPa | 655 MPa | > 485 MPa | 621 MPa | 610 MPa | > 515 MPa | > 515 MPa | > 515 MPa | > 75 ksi | 530 to 730 MPa | > 655 MPa |
| yield strength | 1482 MPa51 | > 205 MPa | > 172 MPa | 205 MPa | 170 MPa | 290 MPa | > 170 MPa | 290 MPa | 290 MPa | > 205 MPa | > 205 MPa | > 205 MPa | > 30 ksi | > 240 MPa | > 345 MPa |
| fatigue strength | 241 MPa52 | no data | no data | 256 MPa | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| fatigue strength | 303 MPa53 | no data | no data | 256 MPa | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| fatigue strength | 379 MPa54 | no data | no data | 256 MPa | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| fatigue strength | 552 MPa55 | no data | no data | 256 MPa | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
| strain hardening exponent | 0.8 -56 | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data | no data |
Why choose it, and why not
Good for
- Springs and clips, where cold-work strength is the main requirement (ATI).
- Light formed structures such as truck and trailer bodies, railway and subway cars and aircraft structural parts (ATI, UPMET).
- Bright decorative and trim parts, which ATI describes as having a bright, attractive surface (ATI).
Watch out for
- Welding and holding at 427 to 816 C, which causes carbide precipitation. Outokumpu prints N/N for intergranular corrosion resistance.
- Chloride pitting: Outokumpu's critical pitting temperature is below 10 C in its test, so chloride exposure is the main corrosion risk.
- Cold work raises magnetic permeability (ATI), so cold-worked parts should not be assumed nonmagnetic.
- Cold-rolled sheet is slightly anisotropic, and the difference is larger in compression (ATI).
Once work hardened, Type 301 has higher tensile strength than other stable austenitic grades (ATI), but it gives up corrosion resistance and welding ease for that strength. Specify it for springs and light formed structures where cold-work strength is the need, and use 304 or 304L where welding matters.
Technical details
For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.
Other names and standards
The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.
| System | Codes |
|---|---|
| UNS | S30100 |
| EN | 1.4310 |
| AISI | 301 |
| JIS | SUS 301 |
| BS | 301S21 |
| AFNOR | Z11 CN 18-08 |
| SS | 2331 |
| GB | 1Cr17Ni7 |
| KS | STS 301 |
| GOST | 07X16H6 |
| ISO | 4310-301-00-I |
| ASTM | A240 (plate, sheet and strip), A666 (plate, sheet and strip) |
| ASME | SA-240 (plate, sheet and strip) |
| AMS | 5901 (sheet and coil) |
| Trade name | ATI 301 |
Notes
The method, full conditions and any caveat for the numbered rows above.
| # | Measurement | Method | Conditions | Caveat |
|---|---|---|---|---|
| 1 | Density | Physical properties table, printed as 0.29 lb/in3 (8.03 g/cm3); specific gravity 8.03 is also printed | temper annealed (the TDS gives its physical values as representative of the annealed condition)temperature not printed | — |
| 2 | Density | Physical properties table, printed as 0.2850 lb/in3 (7.88g/cm3) | form coil and sheet (AMS 5901 datasheet)temperature not printed | — |
| 3 | Density | Physical properties table, printed as 7.9 kg/dm3; kg/dm3 is the same as g/cm3 | temperature room temperature (RT column)unit in source kg/dm3condition not labelled in Table 13 | — |
| 4 | melting point | Physical properties, melting range printed as 2550-2590°F (1399-1421°C); the °C values are used | temperature melting rangetemper annealed (representative values)unit in source 2550-2590 F, printed beside 1399-1421 C | — |
| 5 | elastic modulus | Physical properties, printed as 28 x 10^6 psi (193 GPa) | temper annealed (the TDS says the modulus is lowered in the cold-worked condition)temperature not printed | — |
| 6 | elastic modulus | Physical properties table, modulus of elasticity E in GPa, RT column | temperature room temperature (RT column)condition not labelled in Table 13 | — |
| 7 | Thermal conductivity | Thermal conductivity table, printed as 16.3 W/m•K (9.4 Btu/ft2/hr/F/ft) | temperature 20 to 100 Ctemper annealed (representative values)unit in source W/m•K | — |
| 8 | Thermal conductivity | Thermal conductivity table, printed as 21.4 W/m•K (12.4 Btu/ft2/hr/F/ft) | temperature 20 to 500 Ctemper annealed (representative values)unit in source W/m•K | — |
| 9 | specific heat | Specific heat table, printed as 500 J/kg•K (0.12 Btu/lb/F) | temperature 0 to 100 Ctemper annealed (representative values)unit in source J/kg•K | — |
| 10 | Thermal expansion (CTE) | Linear coefficient of thermal expansion table, printed as 16.6 x 10-6 cm/cm/°C; cm/cm/°C is the same as 1/K | temperature 20 to 100 C meanunit in source 10-6 cm/cm/°C | — |
| 11 | Thermal expansion (CTE) | Linear coefficient of thermal expansion table, printed as 18.6 x 10-6 cm/cm/°C | temperature 20 to 500 C meanunit in source 10-6 cm/cm/°C | — |
| 12 | Thermal expansion (CTE) | Linear coefficient of thermal expansion table, printed as 19.8 x 10-6 cm/cm/°C | temperature 20 to 871 C meanunit in source 10-6 cm/cm/°C | — |
| 13 | electrical resistivity | Electrical resistivity table, printed as 72 Microhm-cm at 20 C (28.3 Microhm-in.) | temperature 20 Ctemper annealed (representative values)unit in source Microhm-cm | — |
| 14 | electrical resistivity | Electrical resistivity table, printed as 100 Microhm-cm at 400 C (39.4 Microhm-in.) | temperature 400 Ctemper annealed (representative values)unit in source Microhm-cm | — |
| 15 | Oxidation resistance limit in air, as printed | Oxidation Resistance section, printed as up to 1550°F (840°C) | temperature up to 840 Cbasis oxidation resistance; the TDS says oxidation depends on atmosphere and design and advises against use at 871 C and aboveunit in source 1550 F (840 C) | — |
| 16 | ultimate tensile strength | Minimum room-temperature mechanical properties table, printed as 75 ksi (515 MPa); UPMET prints the same minimum | temper annealedform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumunit in source 75 ksi | — |
| 17 | ultimate tensile strength | Minimum room-temperature mechanical properties table, printed as 125 ksi (862 MPa); UPMET prints the same minimum | temper 1/4 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumunit in source 125 ksi | — |
| 18 | ultimate tensile strength | Minimum room-temperature mechanical properties table, printed as 150 ksi (1,034 MPa) | temper 1/2 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumunit in source 150 ksi | — |
| 19 | ultimate tensile strength | Minimum room-temperature mechanical properties table, printed as 175 ksi (1,207 MPa) | temper 3/4 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumunit in source 175 ksi | — |
| 20 | ultimate tensile strength | Minimum room-temperature mechanical properties table, printed as 185 ksi (1,276 MPa); UPMET prints the same minimum | temper full hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumunit in source 185 ksi | — |
| 21 | yield strength | Minimum room-temperature mechanical properties table, printed as 30 ksi (205 MPa) | temper annealedform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimum, 0.2 percent offsetunit in source 30 ksi | — |
| 22 | yield strength | Minimum room-temperature mechanical properties table, printed as 75 ksi (517 MPa) | temper 1/4 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimum, 0.2 percent offsetunit in source 75 ksi | — |
| 23 | yield strength | Minimum room-temperature mechanical properties table, printed as 110 ksi (758 MPa) | temper 1/2 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimum, 0.2 percent offsetunit in source 110 ksi | — |
| 24 | yield strength | Minimum room-temperature mechanical properties table, printed as 931 MPa; the ksi figure differs between ATI (125) and UPMET (135), so the MPa value is the one recorded | temper 3/4 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimum, 0.2 percent offsetunit in source ATI prints 125 ksi beside 931 MPa; UPMET prints 135 ksi beside 931 MPa | — |
| 25 | yield strength | Minimum room-temperature mechanical properties table, printed as 140 ksi (965 MPa) | temper full hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimum, 0.2 percent offsetunit in source 140 ksi | — |
| 26 | elongation | Minimum room-temperature mechanical properties table, printed as 40%, Min. | temper annealedform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumgauge 2 in (50 mm) | — |
| 27 | elongation | Minimum room-temperature mechanical properties table, printed as 25% | temper 1/4 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumgauge 2 in (50 mm) | — |
| 28 | elongation | Minimum room-temperature mechanical properties table, printed as 18%, Min. with an asterisk | temper 1/2 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumgauge 2 in (50 mm)thickness greater than 0.015 in (0.038 mm), as the table asterisk states | — |
| 29 | elongation | Minimum room-temperature mechanical properties table, printed as 12%, Min. with an asterisk | temper 3/4 hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumgauge 2 in (50 mm)thickness greater than 0.015 in (0.038 mm), as the table asterisk states | — |
| 30 | elongation | Minimum room-temperature mechanical properties table, printed as 9%, Min. with an asterisk | temper full hardform plate, sheet and strip (ASTM A240 and A666 minimum)basis minimumgauge 2 in (50 mm)thickness greater than 0.015 in (0.038 mm), as the table asterisk states | — |
| 31 | yield strength | Tension table for as-rolled and stress-relieved material, printed as 36 ksi (248 MPa) for longitudinal 0.2% Y.S. | temper annealed (as annealed)orientation longitudinalbasis typicalunit in source 36 ksi | — |
| 32 | yield strength | Tension table, printed as 80 ksi (552 MPa) for longitudinal 0.2% Y.S., as rolled | temper 1/4 hard (as rolled)orientation longitudinalbasis typicalunit in source 80 ksi | — |
| 33 | yield strength | Tension table, printed as 122 ksi (841 MPa) for longitudinal 0.2% Y.S., as rolled | temper 1/2 hard (as rolled)orientation longitudinalbasis typicalunit in source 122 ksi | — |
| 34 | yield strength | Tension table, printed as 142 ksi (979 MPa) for longitudinal 0.2% Y.S., as rolled | temper 3/4 hard (as rolled)orientation longitudinalbasis typicalunit in source 142 ksi | — |
| 35 | yield strength | Tension table, printed as 160 ksi (1,103 MPa) for longitudinal 0.2% Y.S., as rolled | temper full hard (as rolled)orientation longitudinalbasis typicalunit in source 160 ksi | — |
| 36 | elastic modulus | Tension table, elastic modulus printed as 28.0 (193) for longitudinal, as rolled | temper 1/4 hard (as rolled)orientation longitudinalbasis typicalunit in source 28.0 x 10^6 psi (193 GPa) | — |
| 37 | elastic modulus | Tension table, elastic modulus printed as 25.2 (174) for longitudinal, as rolled | temper full hard (as rolled)orientation longitudinalbasis typicalunit in source 25.2 x 10^6 psi (174 GPa) | — |
| 38 | hardness | Typical hardness table, printed as 85 Rb (Rockwell B scale); the Brinell figure for the same row is printed without a unit and is left out | temper annealedbasis typicalunit in source 85 Rb | — |
| 39 | hardness | Typical hardness table, printed as 25 Rc (Rockwell C scale) | temper 1/4 hardbasis typicalunit in source 25 Rc | — |
| 40 | hardness | Typical hardness table, printed as 32 Rc (Rockwell C scale) | temper 1/2 hardbasis typicalunit in source 32 Rc | — |
| 41 | hardness | Typical hardness table, printed as 37 Rc (Rockwell C scale) | temper 3/4 hardbasis typicalunit in source 37 Rc | — |
| 42 | hardness | Typical hardness table, printed as 41 Rc (Rockwell C scale) | temper full hardbasis typicalunit in source 41 Rc | — |
| 43 | ultimate tensile strength | Typical elevated temperature tensile table, Annealed column, 400 F (204 C) row | temper annealedtemperature 204 C (400 F)basis typicalunit in source 80.0 ksi | — |
| 44 | yield strength | Typical elevated temperature tensile table, Annealed yield column, 400 F (204 C) row | temper annealedtemperature 204 C (400 F)basis typical, 0.2 percent offsetunit in source 22.0 ksi | — |
| 45 | ultimate tensile strength | Typical elevated temperature tensile table, Annealed column, 1000 F (538 C) row | temper annealedtemperature 538 C (1000 F)basis typicalunit in source 58.2 ksi | — |
| 46 | yield strength | Typical elevated temperature tensile table, Annealed yield column, 1000 F (538 C) row | temper annealedtemperature 538 C (1000 F)basis typical, 0.2 percent offsetunit in source 18.3 ksi | — |
| 47 | ultimate tensile strength | Typical low temperature tensile table, Annealed row, -320 F (-196 C) line | temper annealedtemperature -196 C (-320 F)basis typicalunit in source 275 ksi | — |
| 48 | yield strength | Typical low temperature tensile table, Annealed row, -320 F (-196 C) line, yield column | temper annealedtemperature -196 C (-320 F)basis typical, 0.2 percent offsetunit in source 75 ksi | — |
| 49 | elongation | Typical low temperature tensile table, Annealed row, -320 F (-196 C) line | temper annealedtemperature -196 C (-320 F)basis typicalgauge 2 in (50 mm) | — |
| 50 | ultimate tensile strength | Typical low temperature tensile table, Full Hard row, -320 F (-196 C) line; the source marks this row with an asterisk | temper full hardtemperature -196 C (-320 F)basis typicalunit in source 302 ksi | — |
| 51 | yield strength | Typical low temperature tensile table, Full Hard row, -320 F (-196 C) line, yield column; the source marks this row with an asterisk | temper full hardtemperature -196 C (-320 F)basis typical, 0.2 percent offsetunit in source 215 ksi | — |
| 52 | fatigue strength | Endurance limit table, printed as 35 ksi (241 MPa) | temper annealedbasis typical endurance limit as printed; test method, cycles and specimen not printedunit in source 35 ksi | — |
| 53 | fatigue strength | Endurance limit table, printed as 44 ksi (303 MPa) | temper 1/4 hardbasis typical endurance limit as printed; test method, cycles and specimen not printedunit in source 44 ksi | — |
| 54 | fatigue strength | Endurance limit table, printed as 55 ksi (379 MPa) | temper 1/2 hardbasis typical endurance limit as printed; test method, cycles and specimen not printedunit in source 55 ksi | — |
| 55 | fatigue strength | Endurance limit table, printed as 80 ksi (552 MPa) | temper full hardbasis typical endurance limit as printed; test method, cycles and specimen not printedunit in source 80 ksi | — |
| 56 | strain hardening exponent | Forming n/Ahom column printed as 0.8/35; footnote 3 defines the first value as the strain-hardening exponent n and the second as homogeneous elongation Ahom, here 35 percent | basis cold forming characteristic from a tension test (Outokumpu footnote 3)temper not labelled in Table 15product 1.4310 row, as printed | — |
Corrosion and compatibility
What happens when it meets other materials and environments.
| Environment | Concern | What happens |
|---|---|---|
| Chloride pitting (critical pitting temperature) | moderate | Critical pitting temperature below 10 C in Outokumpu's potentiostatic test.1 |
| Intergranular corrosion in the delivery and welded conditions | moderate | Outokumpu prints N/N for 1.4310, so it is not resistant to intergranular corrosion in either condition.2 |
| General corrosion in ordinary environments | low | Resists a variety of corrosive media, but less well than the 18-8 chromium-nickel grades (ATI).3 |
| High-temperature oxidation in air | low | Good oxidation resistance up to 840 C; not suggested at 871 C or above.4 |
| # | Environment | Details | Test conditions |
|---|---|---|---|
| 1 | Chloride pitting (critical pitting temperature) | Outokumpu prints a critical pitting temperature below 10 C for 1.4310 (Table 15). Its footnote says this is from potentiostatic testing at +700 mV SCE in 1 M NaCl with the Avesta cell, on a surface ground to P 320 (ASTM G 150). Other methods, such as ASTM G 48, give other values. | test potentiostatic, +700 mV SCE, 1 M NaCl, Avesta cell, surface ground to P 320 (ASTM G 150)temperature critical pitting temperature, below 10 C |
| 2 | Intergranular corrosion in the delivery and welded conditions | Outokumpu prints N/N in the IGC resistance column for 1.4310. Its footnote 6 says Y or N is yes or no for the delivery and welded condition, tested to EN ISO 3651-2. ATI says carbide precipitation during welding restricts 301 in many applications in favour of ATI 304 or 304L. | standard EN 10088-2 test to EN ISO 3651-2condition delivery condition and welded condition |
| 3 | General corrosion in ordinary environments | ATI says 301 is resistant to a variety of corrosive media. However, its corrosion properties are not as good as the 18-8 chromium-nickel steels. | temperature not stated |
| 4 | High-temperature oxidation in air | ATI says 301 has good resistance to oxidation at temperatures up to 1550 F (840 C). At 1600 F (871 C) it gains 10 mg/cm2 in 1000 hours, so it is not suggested for use at 1600 F or above. ATI adds that the oxidation rate depends on the atmosphere and the structural design. | atmosphere air, as printedtime 1000 hours (weight-gain figure at 871 C) |
Risks and side effects
Hazards to people, what happens when a cell overheats, and how the material is handled and stored.
For people
ATI's stainless SDS calls the product an article that does not present a hazard by inhalation or ingestion. Welding and grinding fume and nickel contact are the exposures it names.
- Article
- ATI's SDS for stainless steel, which names ATI301, says the product as an article does not present a hazard to human health by inhalation or ingestion.
- Fume
- Welding, burning, grinding or polishing can release hexavalent chromium, which the SDS says may cause lung, nasal and sinus cancer.
- Skin
- The SDS says nickel-containing alloys may cause sensitization by skin contact. PubChem lists H317 for elemental nickel in 99.9 percent of notifications.
- Exposure limits
- The SDS lists ACGIH limits of 1.5 mg/m3 for nickel and 0.5 mg/m3 for chromium, both as time-weighted averages.
In the environment
Pitting and carbide precipitation are the failure routes. No seawater test for 301 was found.
- Chloride
- Outokumpu's critical pitting temperature for 1.4310 is below 10 C in the Avesta cell test.
- Welds
- ATI says carbide precipitation during welding restricts 301 in many applications in favour of 304 and 304L.
Heat and welding
Holding between 427 and 816 C causes grain-boundary carbide precipitation. Outokumpu prints N/N for intergranular corrosion.
- Range
- ATI says exposure in the 800 to 1500 F (427 to 816 C) range results in grain-boundary carbide precipitation.
- Test
- Outokumpu prints N/N in the intergranular corrosion column for 1.4310: N means no, for the delivery and the welded condition, tested to EN ISO 3651-2.
Test details
The original wording and numbers from the sources, for readers who want them.
Failure risks
| Failure | Trigger and consequence |
|---|---|
| Grain-boundary carbide precipitation after welding or holdinghigh severity | Heating or holding in the 800 to 1500 F (427 to 816 C) range, including welded jointsCarbide precipitation at the grain boundaries lowers corrosion resistance. ATI restricts 301 in welded service in favour of ATI 304 and 304L. |
| Loss of ductility as the temper increasesmoderate severity | Cold rolling from annealed to full hardMinimum elongation falls from 40 percent annealed to 9 percent full hard, with the harder tempers shown for thickness greater than 0.015 in (ATI). |
| Loss of nonmagnetic behaviour with cold workmoderate severity | Cold working, which promotes martensiteMagnetic permeability rises with cold rolling. Properly annealed 301 is completely austenitic (ATI). |
Side effects on surrounding parts
| Affects | Effect |
|---|---|
| Forming and compression loads on cold-rolled parts | Cold-rolled 301 is slightly anisotropic, and the difference is more pronounced in compression. Stress relieving at 371 to 538 C (700 to 1000 F) for 5 minutes to 5 hours makes the material more isotropic (ATI). |
| Magnetic-sensitive hardware | Cold work raises the magnetic permeability of 301 (ATI). |
Handling and storage
- Anneal at 1850 to 2050 F (1010 to 1121 C). Water-quench heavy sections and air-cool thin ones (ATI).
- Outokumpu prints an annealing temperature of 1050 ± 40 C for 1.4310 (A = annealing) and the welding consumable 19 9L.
- Forging: initial 2000 to 2200 F (1093 to 1204 C), finishing at 1700 F (927 C) (ATI).
- The SDS says to use personal protective equipment as required, wear protective gloves, and use respiratory protection when fumes or particulates are generated and exposure limits are exceeded.
Mitigations
- Specify ATI 304 or 304L where welding would otherwise cause carbide precipitation, as ATI recommends.
- Stress relieve cold-rolled parts at 371 to 538 C for 5 minutes to 5 hours. Use the lower temperature and shorter time to limit carbide precipitation (ATI).
- Anneal and cool quickly after cold work. Rapid cooling through the carbide precipitation range keeps the carbides in solution (ATI).
Supply and geography
How common the raw materials are and where they come from.
Nickel production by country
World mine production 3.9 million t of nickel in 2025 (estimated); world reserves more than 140 million t, of which Indonesia holds 62 million t (USGS 2026).
- Top producers (2025)
- Indonesia 66.7%, Philippines 6.9%, Russia 5.1%, New Caledonia 3.6%, Canada 3.6%, China 3.1%
- Recycling
- In 2025 nickel recovered from scrap was about 60 percent of US apparent consumption. Most secondary nickel is stainless-steel scrap (USGS 2026).
- Substitutes
- USGS: low-nickel, duplex or ultrahigh-chromium stainless steels have been substituted for austenitic grades in construction.; USGS: titanium alloys can substitute for nickel or nickel-base alloys in corrosive environments.
Nickel use and US import reliance
Stainless and alloy steel plus nickel-containing alloys typically account for more than 85 percent of US consumption. US net import reliance was 41 percent of apparent consumption in 2025 (estimated).
- Recycling
- Nickel recovered from scrap was about 60 percent of US apparent consumption in 2025.
Chromium production by country
World mine production about 51,000 thousand t gross weight in 2025 (estimated). World resources are greater than 12 billion t of shipping-grade chromite, 95 percent in Kazakhstan and southern Africa (USGS 2026).
- Top producers (2025)
- South Africa 45.1%, Turkey 17.6%, Kazakhstan 13.7%, India 5.9%, Brazil 3.9%, Zimbabwe 3.9%, Finland 3.7%
- Recycling
- Recycled chromium in stainless-steel scrap receipts was 21 percent of US apparent consumption in 2025.
- Substitutes
- USGS: chromium has no substitute in stainless steel, the leading end use.
Chromium import reliance
US net import reliance was 79 percent of apparent consumption in 2025 (estimated). Chromite imports for 2021 to 2024 were from South Africa (96 percent) and Turkey (3 percent) (USGS 2026).
- Recycling
- Recycled chromium was 21 percent of US apparent consumption in 2025.
Documents
Datasheets, safety data sheets, papers and standards you can open.
Full record
The complete spore, as stored. Free to reuse under CC-BY-4.0. Images keep the licence shown with each one.
Show the full YAML
spore: profile
id: stainless-301
spore_version: 0.2
family: stainless-austenitic
name: Stainless steel 301
abbreviation: 301 (UNS S30100)
role: structural and spring alloy
category: metals
type: steels-and-stainless
summary: |
Type 301 is a chromium-nickel austenitic stainless steel, nominally 17 percent chromium and 7 percent nickel (ATI). It gains a great deal of strength when cold rolled: ATI prints minimum tensile strength rising from 515 MPa annealed to 1276 MPa full hard. It is used for springs and for light formed structures such as truck and trailer bodies and railway cars, and it resists corrosion less well than the 18-8 grades (ATI).
best_for: Springs, clips and light formed structures where cold-work strength matters more than corrosion resistance
weakest_at: Chloride pitting (critical pitting temperature below 10 C in Outokumpu's test) and carbide precipitation after welding or holding at 427 to 816 C
identity:
formula: Fe balance, Cr 16.0 to 18.0, Ni 6.0 to 8.0, max 0.15 C, max 2.00 Mn, max 1.00 Si, max 0.045 P, max 0.030 S, max 0.10 N (wt%)
source: upmet-301
where: Chemical Composition table, minimum and maximum by element (UPMET); the ATI product page and ATI data sheet give the same limits except silicon, see gaps
designations:
- system: UNS
code: S30100
source: outokumpu-global
where: Table 4, UNS column, 4310 row
- system: EN
code: '1.4310'
source: outokumpu-global
where: Table 4, EN column, 4310 row
- system: AISI
code: '301'
source: outokumpu-global
where: Table 4, ASTM column (printed as 301), 4310 row
- system: JIS
code: SUS 301
source: outokumpu-global
where: Table 4, JIS column, 4310 row
- system: ISO
code: 4310-301-00-I
source: outokumpu-global
where: Table 5, ISO column, 4310 row
- system: BS
code: 301S21
source: outokumpu-global
where: Table 5, BS/UK column, 4310 row
- system: AFNOR
code: Z11 CN 18-08
source: outokumpu-global
where: Table 5, NF/France column, 4310 row
- system: SS
code: '2331'
source: outokumpu-global
where: Table 5, SS/Sweden column, 4310 row
- system: GB
code: 1Cr17Ni7
source: outokumpu-global
where: Table 5, GB/PR China column, 4310 row
- system: KS
code: STS 301
source: outokumpu-global
where: Table 5, KS/Korea column, 4310 row
- system: GOST
code: 07X16H6
source: outokumpu-global
where: Table 5, GOST/Russia column, 4310 row
- system: ASTM
code: A240
note: plate, sheet and strip
source: ati-301-tds
where: Chemical Composition section, Represented by ASTM A240 and A666
- system: ASTM
code: A666
note: plate, sheet and strip
source: ati-301-tds
where: Chemical Composition section, Represented by ASTM A240 and A666
- system: ASME
code: SA-240
note: plate, sheet and strip
source: ati-301-page
where: Specifications line under the Plate, Sheet and Strip product tables
- system: AMS
code: '5901'
note: sheet and coil
source: upmet-301
where: Title block, AMS 5901 / UNS S30100, datasheet for 301 sheet and coil
- system: Trade name
code: ATI 301
source: ati-301-tds
where: Title block, ATI 301 (UNS S30100)
tags:
environments: []
stresses:
- extreme-cold
applications:
- structures
- mechanisms
properties:
- benchmark: density
value: 8.03
unit: g/cm3
scope: material
conditions:
temper: annealed (the TDS gives its physical values as representative of the annealed condition)
temperature: not printed
method: Physical properties table, printed as 0.29 lb/in3 (8.03 g/cm3); specific gravity 8.03 is also printed
status: ground
source: ati-301-tds
where: Physical Properties, Density row
- benchmark: density
value: 7.88
unit: g/cm3
scope: material
conditions:
form: coil and sheet (AMS 5901 datasheet)
temperature: not printed
method: Physical properties table, printed as 0.2850 lb/in3 (7.88g/cm3)
status: ground
source: upmet-301
where: Physical Properties table, Density row
- benchmark: density
value: 7.9
unit: g/cm3
scope: material
conditions:
temperature: room temperature (RT column)
unit_in_source: kg/dm3
condition: not labelled in Table 13
method: Physical properties table, printed as 7.9 kg/dm3; kg/dm3 is the same as g/cm3
status: ground
source: outokumpu-global
where: Table 13, Density RT column, 4310 row
- benchmark: melting_point
value: 1399
value_high: 1421
bound: range
unit: °C
scope: material
conditions:
temperature: melting range
temper: annealed (representative values)
unit_in_source: 2550-2590 F, printed beside 1399-1421 C
method: Physical properties, melting range printed as 2550-2590°F (1399-1421°C); the °C values are used
status: ground
source: ati-301-tds
where: Physical Properties, Melting Range row
- benchmark: elastic_modulus
value: 193
unit: GPa
scope: material
conditions:
temper: annealed (the TDS says the modulus is lowered in the cold-worked condition)
temperature: not printed
method: Physical properties, printed as 28 x 10^6 psi (193 GPa)
status: ground
source: ati-301-tds
where: Physical Properties, Modulus of Elasticity in Tension row
- benchmark: elastic_modulus
value: 200
unit: GPa
scope: material
conditions:
temperature: room temperature (RT column)
condition: not labelled in Table 13
method: Physical properties table, modulus of elasticity E in GPa, RT column
status: ground
source: outokumpu-global
where: Table 13, Modulus of elasticity RT column, 4310 row
- benchmark: thermal_conductivity
value: 16.3
unit: W/m.K
scope: material
conditions:
temperature: 20 to 100 C
temper: annealed (representative values)
unit_in_source: W/m•K
method: Thermal conductivity table, printed as 16.3 W/m•K (9.4 Btu/ft2/hr/F/ft)
status: ground
source: ati-301-tds
where: Thermal Conductivity table, 20-100 C row
- benchmark: thermal_conductivity
value: 21.4
unit: W/m.K
scope: material
conditions:
temperature: 20 to 500 C
temper: annealed (representative values)
unit_in_source: W/m•K
method: Thermal conductivity table, printed as 21.4 W/m•K (12.4 Btu/ft2/hr/F/ft)
status: ground
source: ati-301-tds
where: Thermal Conductivity table, 20-500 C row
- benchmark: specific_heat
value: 500
unit: J/kg.K
scope: material
conditions:
temperature: 0 to 100 C
temper: annealed (representative values)
unit_in_source: J/kg•K
method: Specific heat table, printed as 500 J/kg•K (0.12 Btu/lb/F)
status: ground
source: ati-301-tds
where: Specific Heat table, 0-100 C row
- benchmark: cte
value: 16.6
unit: 10-6/K
scope: material
conditions:
temperature: 20 to 100 C mean
unit_in_source: 10-6 cm/cm/°C
method: Linear coefficient of thermal expansion table, printed as 16.6 x 10-6 cm/cm/°C; cm/cm/°C is the same as 1/K
status: ground
source: ati-301-tds
where: Linear Coefficient of Thermal Expansion table, 20-100 C row
- benchmark: cte
value: 18.6
unit: 10-6/K
scope: material
conditions:
temperature: 20 to 500 C mean
unit_in_source: 10-6 cm/cm/°C
method: Linear coefficient of thermal expansion table, printed as 18.6 x 10-6 cm/cm/°C
status: ground
source: ati-301-tds
where: Linear Coefficient of Thermal Expansion table, 20-500 C row
- benchmark: cte
value: 19.8
unit: 10-6/K
scope: material
conditions:
temperature: 20 to 871 C mean
unit_in_source: 10-6 cm/cm/°C
method: Linear coefficient of thermal expansion table, printed as 19.8 x 10-6 cm/cm/°C
status: ground
source: ati-301-tds
where: Linear Coefficient of Thermal Expansion table, 20-871 C row
- benchmark: electrical_resistivity
value: 72
unit: µΩ·cm
scope: material
conditions:
temperature: 20 C
temper: annealed (representative values)
unit_in_source: Microhm-cm
method: Electrical resistivity table, printed as 72 Microhm-cm at 20 C (28.3 Microhm-in.)
status: ground
source: ati-301-tds
where: Electrical Resistivity table, 20 C row
- benchmark: electrical_resistivity
value: 100
unit: µΩ·cm
scope: material
conditions:
temperature: 400 C
temper: annealed (representative values)
unit_in_source: Microhm-cm
method: Electrical resistivity table, printed as 100 Microhm-cm at 400 C (39.4 Microhm-in.)
status: ground
source: ati-301-tds
where: Electrical Resistivity table, 400 C row
- benchmark: max_service_temp
label: Oxidation resistance limit in air, as printed
value: 840
unit: °C
scope: material
conditions:
temperature: up to 840 C
basis: oxidation resistance; the TDS says oxidation depends on atmosphere and design and advises against use at 871 C and above
unit_in_source: 1550 F (840 C)
method: Oxidation Resistance section, printed as up to 1550°F (840°C)
status: ground
source: ati-301-tds
where: Oxidation Resistance section
- benchmark: ultimate_tensile_strength
value: 515
unit: MPa
scope: material
conditions:
temper: annealed
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
unit_in_source: 75 ksi
method: Minimum room-temperature mechanical properties table, printed as 75 ksi (515 MPa); UPMET prints the same minimum
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, Annealed row
- benchmark: ultimate_tensile_strength
value: 862
unit: MPa
scope: material
conditions:
temper: 1/4 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
unit_in_source: 125 ksi
method: Minimum room-temperature mechanical properties table, printed as 125 ksi (862 MPa); UPMET prints the same minimum
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 1/4 Hard row
- benchmark: ultimate_tensile_strength
value: 1034
unit: MPa
scope: material
conditions:
temper: 1/2 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
unit_in_source: 150 ksi
method: Minimum room-temperature mechanical properties table, printed as 150 ksi (1,034 MPa)
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 1/2 Hard row
- benchmark: ultimate_tensile_strength
value: 1207
unit: MPa
scope: material
conditions:
temper: 3/4 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
unit_in_source: 175 ksi
method: Minimum room-temperature mechanical properties table, printed as 175 ksi (1,207 MPa)
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 3/4 Hard row
- benchmark: ultimate_tensile_strength
value: 1276
unit: MPa
scope: material
conditions:
temper: full hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
unit_in_source: 185 ksi
method: Minimum room-temperature mechanical properties table, printed as 185 ksi (1,276 MPa); UPMET prints the same minimum
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, Full Hard row
- benchmark: yield_strength
value: 205
unit: MPa
scope: material
conditions:
temper: annealed
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum, 0.2 percent offset
unit_in_source: 30 ksi
method: Minimum room-temperature mechanical properties table, printed as 30 ksi (205 MPa)
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 0.2% Yield column, Annealed row
- benchmark: yield_strength
value: 517
unit: MPa
scope: material
conditions:
temper: 1/4 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum, 0.2 percent offset
unit_in_source: 75 ksi
method: Minimum room-temperature mechanical properties table, printed as 75 ksi (517 MPa)
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 0.2% Yield column, 1/4 Hard row
- benchmark: yield_strength
value: 758
unit: MPa
scope: material
conditions:
temper: 1/2 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum, 0.2 percent offset
unit_in_source: 110 ksi
method: Minimum room-temperature mechanical properties table, printed as 110 ksi (758 MPa)
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 0.2% Yield column, 1/2 Hard row
- benchmark: yield_strength
value: 931
unit: MPa
scope: material
conditions:
temper: 3/4 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum, 0.2 percent offset
unit_in_source: ATI prints 125 ksi beside 931 MPa; UPMET prints 135 ksi beside 931 MPa
method: Minimum room-temperature mechanical properties table, printed as 931 MPa; the ksi figure differs between ATI (125) and UPMET (135), so the MPa value is the one recorded
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 0.2% Yield column, 3/4 Hard row
- benchmark: yield_strength
value: 965
unit: MPa
scope: material
conditions:
temper: full hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum, 0.2 percent offset
unit_in_source: 140 ksi
method: Minimum room-temperature mechanical properties table, printed as 140 ksi (965 MPa)
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, 0.2% Yield column, Full Hard row
- benchmark: elongation
value: 40
unit: '%'
scope: material
conditions:
temper: annealed
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
gauge: 2 in (50 mm)
method: Minimum room-temperature mechanical properties table, printed as 40%, Min.
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, Elong. column, Annealed row
- benchmark: elongation
value: 25
unit: '%'
scope: material
conditions:
temper: 1/4 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
gauge: 2 in (50 mm)
method: Minimum room-temperature mechanical properties table, printed as 25%
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, Elong. column, 1/4 Hard row
- benchmark: elongation
value: 18
unit: '%'
scope: material
conditions:
temper: 1/2 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
gauge: 2 in (50 mm)
thickness: greater than 0.015 in (0.038 mm), as the table asterisk states
method: Minimum room-temperature mechanical properties table, printed as 18%, Min. with an asterisk
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, Elong. column, 1/2 Hard row
- benchmark: elongation
value: 12
unit: '%'
scope: material
conditions:
temper: 3/4 hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
gauge: 2 in (50 mm)
thickness: greater than 0.015 in (0.038 mm), as the table asterisk states
method: Minimum room-temperature mechanical properties table, printed as 12%, Min. with an asterisk
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, Elong. column, 3/4 Hard row
- benchmark: elongation
value: 9
unit: '%'
scope: material
conditions:
temper: full hard
form: plate, sheet and strip (ASTM A240 and A666 minimum)
basis: minimum
gauge: 2 in (50 mm)
thickness: greater than 0.015 in (0.038 mm), as the table asterisk states
method: Minimum room-temperature mechanical properties table, printed as 9%, Min. with an asterisk
status: ground
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table, Elong. column, Full Hard row
- benchmark: yield_strength
value: 248
unit: MPa
scope: material
conditions:
temper: annealed (as annealed)
orientation: longitudinal
basis: typical
unit_in_source: 36 ksi
method: Tension table for as-rolled and stress-relieved material, printed as 36 ksi (248 MPa) for longitudinal 0.2% Y.S.
status: ground
source: ati-301-tds
where: Tension table (as rolled and stress relieved), Longitudinal 0.2% Y.S., Annealed row
- benchmark: yield_strength
value: 552
unit: MPa
scope: material
conditions:
temper: 1/4 hard (as rolled)
orientation: longitudinal
basis: typical
unit_in_source: 80 ksi
method: Tension table, printed as 80 ksi (552 MPa) for longitudinal 0.2% Y.S., as rolled
status: ground
source: ati-301-tds
where: Tension table (as rolled and stress relieved), Longitudinal 0.2% Y.S., 1/4 Hard as rolled row
- benchmark: yield_strength
value: 841
unit: MPa
scope: material
conditions:
temper: 1/2 hard (as rolled)
orientation: longitudinal
basis: typical
unit_in_source: 122 ksi
method: Tension table, printed as 122 ksi (841 MPa) for longitudinal 0.2% Y.S., as rolled
status: ground
source: ati-301-tds
where: Tension table (as rolled and stress relieved), Longitudinal 0.2% Y.S., 1/2 Hard as rolled row
- benchmark: yield_strength
value: 979
unit: MPa
scope: material
conditions:
temper: 3/4 hard (as rolled)
orientation: longitudinal
basis: typical
unit_in_source: 142 ksi
method: Tension table, printed as 142 ksi (979 MPa) for longitudinal 0.2% Y.S., as rolled
status: ground
source: ati-301-tds
where: Tension table (as rolled and stress relieved), Longitudinal 0.2% Y.S., 3/4 Hard as rolled row
- benchmark: yield_strength
value: 1103
unit: MPa
scope: material
conditions:
temper: full hard (as rolled)
orientation: longitudinal
basis: typical
unit_in_source: 160 ksi
method: Tension table, printed as 160 ksi (1,103 MPa) for longitudinal 0.2% Y.S., as rolled
status: ground
source: ati-301-tds
where: Tension table (as rolled and stress relieved), Longitudinal 0.2% Y.S., Full Hard as rolled row
- benchmark: elastic_modulus
value: 193
unit: GPa
scope: material
conditions:
temper: 1/4 hard (as rolled)
orientation: longitudinal
basis: typical
unit_in_source: 28.0 x 10^6 psi (193 GPa)
method: Tension table, elastic modulus printed as 28.0 (193) for longitudinal, as rolled
status: ground
source: ati-301-tds
where: Tension table (as rolled and stress relieved), Longitudinal Elastic Modulus, 1/4 Hard as rolled row
- benchmark: elastic_modulus
value: 174
unit: GPa
scope: material
conditions:
temper: full hard (as rolled)
orientation: longitudinal
basis: typical
unit_in_source: 25.2 x 10^6 psi (174 GPa)
method: Tension table, elastic modulus printed as 25.2 (174) for longitudinal, as rolled
status: ground
source: ati-301-tds
where: Tension table (as rolled and stress relieved), Longitudinal Elastic Modulus, Full Hard as rolled row
- benchmark: hardness
value: 85
unit: HRB
scope: material
conditions:
temper: annealed
basis: typical
unit_in_source: 85 Rb
method: Typical hardness table, printed as 85 Rb (Rockwell B scale); the Brinell figure for the same row is printed without a unit and is left out
status: ground
source: ati-301-tds
where: Hardness table, Annealed row
- benchmark: hardness
value: 25
unit: HRC
scope: material
conditions:
temper: 1/4 hard
basis: typical
unit_in_source: 25 Rc
method: Typical hardness table, printed as 25 Rc (Rockwell C scale)
status: ground
source: ati-301-tds
where: Hardness table, 1/4 Hard row
- benchmark: hardness
value: 32
unit: HRC
scope: material
conditions:
temper: 1/2 hard
basis: typical
unit_in_source: 32 Rc
method: Typical hardness table, printed as 32 Rc (Rockwell C scale)
status: ground
source: ati-301-tds
where: Hardness table, 1/2 Hard row
- benchmark: hardness
value: 37
unit: HRC
scope: material
conditions:
temper: 3/4 hard
basis: typical
unit_in_source: 37 Rc
method: Typical hardness table, printed as 37 Rc (Rockwell C scale)
status: ground
source: ati-301-tds
where: Hardness table, 3/4 Hard row
- benchmark: hardness
value: 41
unit: HRC
scope: material
conditions:
temper: full hard
basis: typical
unit_in_source: 41 Rc
method: Typical hardness table, printed as 41 Rc (Rockwell C scale)
status: ground
source: ati-301-tds
where: Hardness table, Full Hard row
- benchmark: ultimate_tensile_strength
value: 552
unit: MPa
scope: material
conditions:
temper: annealed
temperature: 204 C (400 F)
basis: typical
unit_in_source: 80.0 ksi
method: Typical elevated temperature tensile table, Annealed column, 400 F (204 C) row
status: ground
source: ati-301-tds
where: Typical Elevated Temperature Tensile Properties table, 400 (204) row
- benchmark: yield_strength
value: 152
unit: MPa
scope: material
conditions:
temper: annealed
temperature: 204 C (400 F)
basis: typical, 0.2 percent offset
unit_in_source: 22.0 ksi
method: Typical elevated temperature tensile table, Annealed yield column, 400 F (204 C) row
status: ground
source: ati-301-tds
where: Typical Elevated Temperature Tensile Properties table, 400 (204) row, yield column
- benchmark: ultimate_tensile_strength
value: 401
unit: MPa
scope: material
conditions:
temper: annealed
temperature: 538 C (1000 F)
basis: typical
unit_in_source: 58.2 ksi
method: Typical elevated temperature tensile table, Annealed column, 1000 F (538 C) row
status: ground
source: ati-301-tds
where: Typical Elevated Temperature Tensile Properties table, 1000 (538) row
- benchmark: yield_strength
value: 126
unit: MPa
scope: material
conditions:
temper: annealed
temperature: 538 C (1000 F)
basis: typical, 0.2 percent offset
unit_in_source: 18.3 ksi
method: Typical elevated temperature tensile table, Annealed yield column, 1000 F (538 C) row
status: ground
source: ati-301-tds
where: Typical Elevated Temperature Tensile Properties table, 1000 (538) row, yield column
- benchmark: ultimate_tensile_strength
value: 1896
unit: MPa
scope: material
conditions:
temper: annealed
temperature: '-196 C (-320 F)'
basis: typical
unit_in_source: 275 ksi
method: Typical low temperature tensile table, Annealed row, -320 F (-196 C) line
status: ground
source: ati-301-tds
where: Typical Low Temperature Tensile Properties table, Annealed row, -320 (-196) line
- benchmark: yield_strength
value: 517
unit: MPa
scope: material
conditions:
temper: annealed
temperature: '-196 C (-320 F)'
basis: typical, 0.2 percent offset
unit_in_source: 75 ksi
method: Typical low temperature tensile table, Annealed row, -320 F (-196 C) line, yield column
status: ground
source: ati-301-tds
where: Typical Low Temperature Tensile Properties table, Annealed row, -320 (-196) line
- benchmark: elongation
value: 30
unit: '%'
scope: material
conditions:
temper: annealed
temperature: '-196 C (-320 F)'
basis: typical
gauge: 2 in (50 mm)
method: Typical low temperature tensile table, Annealed row, -320 F (-196 C) line
status: ground
source: ati-301-tds
where: Typical Low Temperature Tensile Properties table, Annealed row, -320 (-196) line
- benchmark: ultimate_tensile_strength
value: 2082
unit: MPa
scope: material
conditions:
temper: full hard
temperature: '-196 C (-320 F)'
basis: typical
unit_in_source: 302 ksi
method: Typical low temperature tensile table, Full Hard row, -320 F (-196 C) line; the source marks this row with an asterisk
status: ground
source: ati-301-tds
where: Typical Low Temperature Tensile Properties table, Full Hard row, -320 (-196) line
- benchmark: yield_strength
value: 1482
unit: MPa
scope: material
conditions:
temper: full hard
temperature: '-196 C (-320 F)'
basis: typical, 0.2 percent offset
unit_in_source: 215 ksi
method: Typical low temperature tensile table, Full Hard row, -320 F (-196 C) line, yield column; the source marks this row with an asterisk
status: ground
source: ati-301-tds
where: Typical Low Temperature Tensile Properties table, Full Hard row, -320 (-196) line, yield column
- benchmark: fatigue_strength
value: 241
unit: MPa
scope: material
conditions:
temper: annealed
basis: typical endurance limit as printed; test method, cycles and specimen not printed
unit_in_source: 35 ksi
method: Endurance limit table, printed as 35 ksi (241 MPa)
status: ground
source: ati-301-tds
where: Fatigue Strength section, Endurance Limit table, Annealed row
- benchmark: fatigue_strength
value: 303
unit: MPa
scope: material
conditions:
temper: 1/4 hard
basis: typical endurance limit as printed; test method, cycles and specimen not printed
unit_in_source: 44 ksi
method: Endurance limit table, printed as 44 ksi (303 MPa)
status: ground
source: ati-301-tds
where: Fatigue Strength section, Endurance Limit table, 1/4 Hard row
- benchmark: fatigue_strength
value: 379
unit: MPa
scope: material
conditions:
temper: 1/2 hard
basis: typical endurance limit as printed; test method, cycles and specimen not printed
unit_in_source: 55 ksi
method: Endurance limit table, printed as 55 ksi (379 MPa)
status: ground
source: ati-301-tds
where: Fatigue Strength section, Endurance Limit table, 1/2 Hard row
- benchmark: fatigue_strength
value: 552
unit: MPa
scope: material
conditions:
temper: full hard
basis: typical endurance limit as printed; test method, cycles and specimen not printed
unit_in_source: 80 ksi
method: Endurance limit table, printed as 80 ksi (552 MPa)
status: ground
source: ati-301-tds
where: Fatigue Strength section, Endurance Limit table, Full Hard row
- benchmark: strain_hardening_exponent
value: 0.8
unit: '-'
scope: material
conditions:
basis: cold forming characteristic from a tension test (Outokumpu footnote 3)
temper: not labelled in Table 15
product: 1.4310 row, as printed
method: Forming n/Ahom column printed as 0.8/35; footnote 3 defines the first value as the strain-hardening exponent n and the second as homogeneous elongation Ahom, here 35 percent
status: ground
source: outokumpu-global
where: Table 15 (fabrication and use characteristics), Forming n/Ahom column, 4310 row
corrosion:
- environment: Chloride pitting (critical pitting temperature)
headline: Critical pitting temperature below 10 C in Outokumpu's potentiostatic test.
effect: Outokumpu prints a critical pitting temperature below 10 C for 1.4310 (Table 15). Its footnote says this is from potentiostatic testing at +700 mV SCE in 1 M NaCl with the Avesta cell, on a surface ground to P 320 (ASTM G 150). Other methods, such as ASTM G 48, give other values.
rating: moderate
conditions:
test: potentiostatic, +700 mV SCE, 1 M NaCl, Avesta cell, surface ground to P 320 (ASTM G 150)
temperature: critical pitting temperature, below 10 C
source: outokumpu-global
where: Table 15, CPT column (footnote 7), 4310 row
- environment: Intergranular corrosion in the delivery and welded conditions
headline: Outokumpu prints N/N for 1.4310, so it is not resistant to intergranular corrosion in either condition.
effect: Outokumpu prints N/N in the IGC resistance column for 1.4310. Its footnote 6 says Y or N is yes or no for the delivery and welded condition, tested to EN ISO 3651-2. ATI says carbide precipitation during welding restricts 301 in many applications in favour of ATI 304 or 304L.
rating: moderate
conditions:
standard: EN 10088-2 test to EN ISO 3651-2
condition: delivery condition and welded condition
source: outokumpu-global
where: Table 15, IGC resistance column (footnote 6), 4310 row
- environment: General corrosion in ordinary environments
headline: Resists a variety of corrosive media, but less well than the 18-8 chromium-nickel grades (ATI).
effect: ATI says 301 is resistant to a variety of corrosive media. However, its corrosion properties are not as good as the 18-8 chromium-nickel steels.
rating: low
conditions:
temperature: not stated
source: ati-301-tds
where: Corrosion Resistance section
- environment: High-temperature oxidation in air
headline: Good oxidation resistance up to 840 C; not suggested at 871 C or above.
effect: ATI says 301 has good resistance to oxidation at temperatures up to 1550 F (840 C). At 1600 F (871 C) it gains 10 mg/cm2 in 1000 hours, so it is not suggested for use at 1600 F or above. ATI adds that the oxidation rate depends on the atmosphere and the structural design.
rating: low
conditions:
atmosphere: air, as printed
time: 1000 hours (weight-gain figure at 871 C)
source: ati-301-tds
where: Oxidation Resistance section
risks:
hazards:
- text: 'ATI''s stainless steel safety data sheet FRP008, which names ATI301, is classed Danger. Its hazard statements are: May cause cancer; May cause an allergic skin reaction; Causes damage to the respiratory tract through prolonged or repeated exposure if inhaled. It also says the product is an article and does not present a hazard to human health by inhalation or ingestion.'
ghs: []
source: ati-frp008-sds
where: Section 2, Hazards Identification (hazard statements and article statement)
- text: The SDS says welding, burning, melting, sawing, brazing, grinding, buffing or polishing can release hexavalent chromium (Chromium VI), which may cause lung, nasal and/or sinus cancer, along with other fumes the SDS lists.
ghs: []
source: ati-frp008-sds
where: Section 2, Hazards not otherwise classified; Section 5, Hazardous combustion products
- text: The SDS says nickel- or cobalt-containing alloys may cause sensitization by skin contact.
ghs: []
source: ati-frp008-sds
where: Section 11, Toxicological Information, Skin contact and Sensitization
- text: 'SDS exposure limits for the constituent metals: nickel, ACGIH TWA 1.5 mg/m3 (inhalable fraction) and OSHA PEL TWA 1 mg/m3; chromium, ACGIH TWA 0.5 mg/m3 and OSHA PEL TWA 1 mg/m3. The table is for the product family, not 301 alone.'
ghs: []
source: ati-frp008-sds
where: Section 8, Exposure Controls, ACGIH TLV and OSHA PEL table
- text: PubChem aggregated notifications for elemental nickel include H317 (99.9 percent of notifications), H372 (99.7 percent), H351 (72.9 percent) and H412 (47.2 percent), with signal word Danger. These describe the element, not the 301 alloy.
ghs:
- H317
- H372
- H351
- H412
source: pubchem-nickel
where: GHS Classification, ECHA C&L aggregated notifications (CID 935)
- text: PubChem aggregated notifications for elemental chromium include H317 (20.7 percent), H319 (19.1 percent) and H334 (20.3 percent), with signal word Danger. The record says it does not meet GHS criteria for 50 percent of reports, and it describes the element, not the 301 alloy.
ghs:
- H317
- H319
- H334
source: pubchem-chromium
where: GHS Classification, ECHA C&L aggregated notifications (CID 23976)
failure_risks:
- mode: Grain-boundary carbide precipitation after welding or holding
trigger: Heating or holding in the 800 to 1500 F (427 to 816 C) range, including welded joints
consequence: Carbide precipitation at the grain boundaries lowers corrosion resistance. ATI restricts 301 in welded service in favour of ATI 304 and 304L.
severity: high
source: ati-301-tds
where: Corrosion Resistance section and Structure paragraph of the Heat Treatment section
- mode: Loss of ductility as the temper increases
trigger: Cold rolling from annealed to full hard
consequence: Minimum elongation falls from 40 percent annealed to 9 percent full hard, with the harder tempers shown for thickness greater than 0.015 in (ATI).
severity: moderate
source: ati-301-tds
where: Minimum Room Temperature Mechanical Properties table
- mode: Loss of nonmagnetic behaviour with cold work
trigger: Cold working, which promotes martensite
consequence: Magnetic permeability rises with cold rolling. Properly annealed 301 is completely austenitic (ATI).
severity: moderate
source: ati-301-tds
where: Magnetic Permeability section
side_effects:
- text: Cold-rolled 301 is slightly anisotropic, and the difference is more pronounced in compression. Stress relieving at 371 to 538 C (700 to 1000 F) for 5 minutes to 5 hours makes the material more isotropic (ATI).
affects: Forming and compression loads on cold-rolled parts
source: ati-301-tds
where: Mechanical Properties section, text before the as-rolled table
- text: Cold work raises the magnetic permeability of 301 (ATI).
affects: Magnetic-sensitive hardware
source: ati-301-tds
where: Magnetic Permeability section
handling:
- text: Anneal at 1850 to 2050 F (1010 to 1121 C). Water-quench heavy sections and air-cool thin ones (ATI).
source: ati-301-tds
where: Heat Treatment section, Annealing Temperature
- text: Outokumpu prints an annealing temperature of 1050 ± 40 C for 1.4310 (A = annealing) and the welding consumable 19 9L.
source: outokumpu-global
where: Table 15 (fabrication), heat treatment and welding columns, 4310 row
- text: 'Forging: initial 2000 to 2200 F (1093 to 1204 C), finishing at 1700 F (927 C) (ATI).'
source: ati-301-tds
where: Heat Treatment section, Forging Treatment
- text: The SDS says to use personal protective equipment as required, wear protective gloves, and use respiratory protection when fumes or particulates are generated and exposure limits are exceeded.
source: ati-frp008-sds
where: Section 2, Precautionary Statements; Section 8, Respiratory protection
mitigations:
- text: Specify ATI 304 or 304L where welding would otherwise cause carbide precipitation, as ATI recommends.
source: ati-301-tds
where: Corrosion Resistance section
- text: Stress relieve cold-rolled parts at 371 to 538 C for 5 minutes to 5 hours. Use the lower temperature and shorter time to limit carbide precipitation (ATI).
source: ati-301-tds
where: Mechanical Properties section
- text: Anneal and cool quickly after cold work. Rapid cooling through the carbide precipitation range keeps the carbides in solution (ATI).
source: ati-301-tds
where: Heat Treatment section, Annealing Temperature
uses:
- application: structures
device: Aircraft structural parts
example: UPMET lists aircraft structural parts among the industry applications for its 301 sheet and coil. It also lists trailer bodies, architectural parts and conveyor parts.
source: upmet-301
where: Industry Applications list
- application: structures
device: Truck and trailer bodies, railway and subway cars
example: ATI names truck and trailer bodies and railway and subway cars among the major applications for 301.
source: ati-301-tds
where: General Properties section, first paragraph
- application: mechanisms
device: Springs and hose clamps
example: ATI names springs and hose clamps among the major applications for 301.
source: ati-301-tds
where: General Properties section, first paragraph
supply:
- subject: Nickel production by country
abundance: World mine production 3.9 million t of nickel in 2025 (estimated); world reserves more than 140 million t, of which Indonesia holds 62 million t (USGS 2026).
producers:
- country: Indonesia
share_percent: 66.7
year: 2025
basis: 2,600,000 t of 3,900,000 t world total (2025e), computed
- country: Philippines
share_percent: 6.9
year: 2025
basis: 270,000 t of 3,900,000 t, computed
- country: Russia
share_percent: 5.1
year: 2025
basis: 200,000 t of 3,900,000 t, computed
- country: New Caledonia
share_percent: 3.6
year: 2025
basis: 140,000 t of 3,900,000 t, computed
- country: Canada
share_percent: 3.6
year: 2025
basis: 140,000 t of 3,900,000 t, computed
- country: China
share_percent: 3.1
year: 2025
basis: 120,000 t of 3,900,000 t, computed
critical_lists: []
recycling: In 2025 nickel recovered from scrap was about 60 percent of US apparent consumption. Most secondary nickel is stainless-steel scrap (USGS 2026).
substitutes:
- 'USGS: low-nickel, duplex or ultrahigh-chromium stainless steels have been substituted for austenitic grades in construction.'
- 'USGS: titanium alloys can substitute for nickel or nickel-base alloys in corrosive environments.'
source: usgs-nickel-2026
where: World Mine Production and Reserves table (2025e); Recycling; Substitutes
- subject: Nickel use and US import reliance
abundance: Stainless and alloy steel plus nickel-containing alloys typically account for more than 85 percent of US consumption. US net import reliance was 41 percent of apparent consumption in 2025 (estimated).
producers: []
critical_lists: []
recycling: Nickel recovered from scrap was about 60 percent of US apparent consumption in 2025.
substitutes: []
source: usgs-nickel-2026
where: Domestic Production and Use; Salient Statistics (net import reliance row)
- subject: Chromium production by country
abundance: World mine production about 51,000 thousand t gross weight in 2025 (estimated). World resources are greater than 12 billion t of shipping-grade chromite, 95 percent in Kazakhstan and southern Africa (USGS 2026).
producers:
- country: South Africa
share_percent: 45.1
year: 2025
basis: 23,000 of 51,000 thousand t gross weight (2025e), computed
- country: Turkey
share_percent: 17.6
year: 2025
basis: 9,000 of 51,000 thousand t, computed
- country: Kazakhstan
share_percent: 13.7
year: 2025
basis: 7,000 of 51,000 thousand t, computed
- country: India
share_percent: 5.9
year: 2025
basis: 3,000 of 51,000 thousand t, computed
- country: Brazil
share_percent: 3.9
year: 2025
basis: 2,000 of 51,000 thousand t, computed
- country: Zimbabwe
share_percent: 3.9
year: 2025
basis: 2,000 of 51,000 thousand t, computed
- country: Finland
share_percent: 3.7
year: 2025
basis: 1,900 of 51,000 thousand t, computed
critical_lists: []
recycling: Recycled chromium in stainless-steel scrap receipts was 21 percent of US apparent consumption in 2025.
substitutes:
- 'USGS: chromium has no substitute in stainless steel, the leading end use.'
source: usgs-chromium-2026
where: World Mine Production and Reserves table (2025e, gross weight); World Resources; Substitutes; Recycling
- subject: Chromium import reliance
abundance: US net import reliance was 79 percent of apparent consumption in 2025 (estimated). Chromite imports for 2021 to 2024 were from South Africa (96 percent) and Turkey (3 percent) (USGS 2026).
producers: []
critical_lists: []
recycling: Recycled chromium was 21 percent of US apparent consumption in 2025.
substitutes: []
source: usgs-chromium-2026
where: Salient Statistics (net import reliance row); Import Sources (2021-24)
media: []
documents:
- title: ATI 301 Technical Data Sheet, version 1 (2014)
type: datasheet
url: https://atimaterials.com/Products/Documents/datasheets/stainless-specialty-steel/austenitic/ati_301_tds_en_v1.pdf
year: 2014
- title: ATI 301 product page (composition, specifications and minimum properties)
type: datasheet
url: https://atimaterials.com/Products/ati-301
- title: 'UPMET: Datasheet for 301 Stainless Steel Sheet and Coil, AMS 5901 (UNS S30100)'
type: datasheet
url: https://www.upmet.com/sites/default/files/datasheets/301.pdf
year: 2026
- title: 'Outokumpu: Steel Grades, Properties and Global Standards (Tables 4, 5, 13 and 15)'
type: datasheet
url: https://www.outokumpu.com/-/media/from-sharepoint/documents/product/outokumpu-steel-grades-properties-global-standards.pdf
- title: ATI Stainless Steel Safety Data Sheet FRP008 (covers ATI301), revision date 04-Sep-2018
type: sds
url: https://atimaterials.com/safety-data-sheets/Documents/NorthAmerica/NA-EN/FRP/FRP008%20Stainless%20Steel%20NA-EN%20Rev5.pdf
year: 2018
- title: 'USGS Mineral Commodity Summaries 2026: Nickel'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
year: 2026
- title: 'USGS Mineral Commodity Summaries 2026: Chromium'
type: report
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-chromium.pdf
year: 2026
- title: 'PubChem: Nickel (CID 935), UN GHS classification'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/rest/pug_view/data/compound/935/JSON
year: 2026
- title: 'PubChem: Chromium (CID 23976), UN GHS classification'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/rest/pug_view/data/compound/23976/JSON
year: 2026
gaps:
- No ASTM A240 or A666 standard text was read. The minimum temper values come from the ATI and UPMET tables that cite those specifications.
- The EN steel name is not printed on any page read in this run; only the material number 1.4310 is. No DIN or SAE steel name was printed on the pages read.
- Hardness is not in the canonical property list, so the name hardness is used. The Brinell figures in the ATI typical hardness table are printed without a unit and are left out.
- Strain-hardening exponent is not in the canonical property list, so the name strain_hardening_exponent is used. Magnetic permeability is not in the list either; only the effect of cold work is recorded, from ATI.
- The 3/4 hard yield strength is printed as 125 ksi by ATI and as 135 ksi by UPMET, both beside 931 MPa. The MPa value is recorded and the conflict is noted in the method.
- Silicon is printed as a maximum of 0.75 percent in the 2014 ATI data sheet and 1.00 percent on the ATI product page and in the UPMET datasheet. The recipe uses 1.00.
- Outokumpu's Table 7 and Table 9 minimum values for 1.4310 carry no temper label, so they are not used. The elevated and low temperature values come from ATI's annealed and full-hard rows only.
- ATI's typical Charpy impact values (150 J at -196 C) are printed without a temper label, so they are not in the file.
- Critical-mineral lists (USGS 2025 final list and the EU list) were not opened in this run, so critical_lists is empty for nickel and chromium.
- No space or flight source for 301 was found. UPMET lists Space among related industries but names no space part, so the uses come from the ATI and UPMET application lists.
- No NASA or NIST cryogenic source for 301 was used. NIST NBSIR 80-1627 was fetched and has no AISI 301 data.
- Hazard lines from the ATI stainless SDS (FRP008) cover the product family, which includes ATI301, so they are not 301-only figures. The PubChem records are for the elements.
- Web search was unavailable in this run because the search budget for the turn was used up. Sources are the pages reached from the first URLs and their links. The AK Steel 301 data sheet host did not resolve, the Carpenter SDS returned 404, and the Swiss Steel 1.4310 page held no 1.4310 data.
- Chloride and seawater data for 301 beyond the Outokumpu critical pitting temperature could not be located in the pages read. No ASTM G 48 value for 301 could be located either.
- Fatigue values are typical endurance limits as printed; the test method, cycles and specimen are not stated in the source.
sources:
ati-301-tds:
title: 'ATI 301 Technical Data Sheet, Stainless Steel: Austenitic (UNS S30100), version 1 dated 2/17/2014'
id: ATI 301 TDS version 1
url: https://atimaterials.com/Products/Documents/datasheets/stainless-specialty-steel/austenitic/ati_301_tds_en_v1.pdf
kind: datasheet
year: 2014
license: cited, not reproduced
ati-301-page:
title: ATI 301 austenitic stainless steel product page (composition, specifications, minimum properties)
id: ati-301
url: https://atimaterials.com/Products/ati-301
kind: datasheet
license: cited, not reproduced
upmet-301:
title: 'United Performance Metals: Datasheet for 301 Stainless Steel Sheet and Coil, AMS 5901 (UNS S30100)'
id: 301.pdf
url: https://www.upmet.com/sites/default/files/datasheets/301.pdf
kind: datasheet
year: 2026
license: cited, not reproduced
outokumpu-global:
title: 'Outokumpu: Steel Grades, Properties and Global Standards (Tables 4, 5, 13 and 15)'
id: outokumpu-steel-grades-properties-global-standards.pdf
url: https://www.outokumpu.com/-/media/from-sharepoint/documents/product/outokumpu-steel-grades-properties-global-standards.pdf
kind: handbook
license: cited, not reproduced
ati-frp008-sds:
title: ATI Stainless Steel Safety Data Sheet FRP008 (North America, revision date 04-Sep-2018, covers ATI301)
id: FRP008
url: https://atimaterials.com/safety-data-sheets/Documents/NorthAmerica/NA-EN/FRP/FRP008%20Stainless%20Steel%20NA-EN%20Rev5.pdf
kind: datasheet
year: 2018
license: supplier document, linked not reproduced
usgs-nickel-2026:
title: 'USGS Mineral Commodity Summaries 2026: Nickel'
id: mcs2026-nickel
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-nickel.pdf
kind: report
year: 2026
license: public domain
usgs-chromium-2026:
title: 'USGS Mineral Commodity Summaries 2026: Chromium'
id: mcs2026-chromium
url: https://pubs.usgs.gov/periodicals/mcs2026/mcs2026-chromium.pdf
kind: report
year: 2026
license: public domain
pubchem-nickel:
title: 'PubChem: Nickel (CID 935), UN GHS classification'
id: CID 935
url: https://pubchem.ncbi.nlm.nih.gov/rest/pug_view/data/compound/935/JSON
kind: database
license: PubChem terms (public)
pubchem-chromium:
title: 'PubChem: Chromium (CID 23976), UN GHS classification'
id: CID 23976
url: https://pubchem.ncbi.nlm.nih.gov/rest/pug_view/data/compound/23976/JSON
kind: database
license: PubChem terms (public)
license: CC-BY-4.0
updated: '2026-10-24'
review:
status: draft
method: assistant
checked_values: 56
unreachable: 0
caveats: 3
note: 'Read by an AI assistant on 2026-10-24 from pages fetched in this run: the ATI 301 technical data sheet (version 1, 2014) and ATI 301 product page, the UPMET 301 datasheet (AMS 5901), Outokumpu''s steel grades handbook (Tables 4, 5, 13 and 15), ATI''s stainless steel SDS FRP008, USGS Mineral Commodity Summaries 2026 for nickel and chromium, and PubChem nickel and chromium records. Web search was unavailable in this run.'
story:
recipe:
line: 'Type 301 is an iron-based austenitic stainless steel. ATI and UPMET give the same composition limits: 16 to 18 percent chromium and 6 to 8 percent nickel, with maximum limits on carbon, manganese, silicon, phosphorus, sulfur and nitrogen, and iron as the balance. It is sold as cold-rolled strip, sheet and plate, and its temper, from annealed to full hard, is set by how much it is cold rolled (ATI).'
parts:
- name: Iron
symbol: Fe
share_note: balance (the rest)
role: The matrix of the alloy. It holds the austenite structure that gives 301 its ductility.
- name: Chromium
symbol: Cr
share_percent: 16
share_high: 18
source: upmet-301
where: Chemical Composition table, Cr row (minimum and maximum)
role: Forms the passive oxide film that gives corrosion resistance.
- name: Nickel
symbol: Ni
share_percent: 6
share_high: 8
source: upmet-301
where: Chemical Composition table, Ni row (minimum and maximum)
role: Holds the austenite structure at room temperature.
- name: Manganese
symbol: Mn
share_percent: 0
share_high: 2
source: upmet-301
where: Chemical Composition table, Mn row (maximum)
role: Deoxidiser in the melt; the printed limit is a maximum.
- name: Silicon
symbol: Si
share_percent: 0
share_high: 1
source: upmet-301
where: Chemical Composition table, Si row (maximum 1.00); the 2014 ATI data sheet prints 0.75
role: Deoxidiser in the melt; the printed limit is a maximum.
- name: Carbon
symbol: C
share_percent: 0
share_high: 0.15
source: upmet-301
where: Chemical Composition table, C row (maximum)
role: Adds strength, but chromium carbide can form at the grain boundaries when the steel is held between 427 and 816 C (ATI).
- name: Nitrogen
symbol: 'N'
share_percent: 0
share_high: 0.1
source: upmet-301
where: Chemical Composition table, N row (maximum 0.10)
role: Held to a maximum; it adds strength in austenite.
- name: Phosphorus
symbol: P
share_percent: 0
share_high: 0.045
source: upmet-301
where: Chemical Composition table, P row (maximum 0.045)
role: Impurity held low.
- name: Sulfur
symbol: S
share_percent: 0
share_high: 0.03
source: upmet-301
where: Chemical Composition table, S row (maximum 0.030)
role: Impurity held low.
risk_groups:
- title: For people
level: 1
verdict: Fume and skin contact are the hazards
lead: ATI's stainless SDS calls the product an article that does not present a hazard by inhalation or ingestion. Welding and grinding fume and nickel contact are the exposures it names.
points:
- label: Article
line: ATI's SDS for stainless steel, which names ATI301, says the product as an article does not present a hazard to human health by inhalation or ingestion.
- label: Fume
line: Welding, burning, grinding or polishing can release hexavalent chromium, which the SDS says may cause lung, nasal and sinus cancer.
- label: Skin
line: The SDS says nickel-containing alloys may cause sensitization by skin contact. PubChem lists H317 for elemental nickel in 99.9 percent of notifications.
- label: Exposure limits
line: The SDS lists ACGIH limits of 1.5 mg/m3 for nickel and 0.5 mg/m3 for chromium, both as time-weighted averages.
- title: In the environment
level: 2
verdict: Chloride and welds are the watch points
lead: Pitting and carbide precipitation are the failure routes. No seawater test for 301 was found.
points:
- label: Chloride
line: Outokumpu's critical pitting temperature for 1.4310 is below 10 C in the Avesta cell test.
- label: Welds
line: ATI says carbide precipitation during welding restricts 301 in many applications in favour of 304 and 304L.
- title: Heat and welding
level: 2
verdict: Heat history sets the risk
lead: Holding between 427 and 816 C causes grain-boundary carbide precipitation. Outokumpu prints N/N for intergranular corrosion.
points:
- label: Range
line: ATI says exposure in the 800 to 1500 F (427 to 816 C) range results in grain-boundary carbide precipitation.
- label: Test
line: 'Outokumpu prints N/N in the intergranular corrosion column for 1.4310: N means no, for the delivery and the welded condition, tested to EN ISO 3651-2.'
why: Type 301 is the cold-work grade of the stainless family. ATI says its tensile strength in the work-hardened condition is higher than other stable austenitic grades, and ATI and UPMET list springs, aircraft structural parts, truck and trailer bodies and railway cars as uses. Its limits are corrosion resistance below the 18-8 grades and carbide precipitation on welding.
uses:
- where: Aircraft structural parts
line: UPMET lists aircraft structural parts among the industry applications for its 301 sheet and coil. It also lists trailer bodies, architectural parts and conveyor parts.
- where: Truck and trailer bodies, railway and subway cars
line: ATI names truck and trailer bodies and railway and subway cars among the major applications for 301.
- where: Springs
line: ATI names springs and hose clamps among the major applications for 301, alongside automobile trim and kitchen equipment.
can_do:
- label: Strength by temper
benchmark: ultimate_tensile_strength
line: Minimum tensile strength is 515 MPa annealed, 862 MPa quarter hard, 1034 MPa half hard, 1207 MPa three-quarter hard and 1276 MPa full hard (ASTM A240 and A666 minimums, ATI).
- label: Yield by temper
benchmark: yield_strength
line: Minimum yield strength is 205 MPa annealed and 965 MPa full hard (ATI). The three-quarter hard minimum is 931 MPa.
- label: How fast it work hardens
benchmark: strain_hardening_exponent
line: Typical as-rolled yield rises from 248 MPa annealed to 552 MPa quarter hard and 1103 MPa full hard (ATI). Outokumpu prints a strain-hardening exponent of 0.8 for 1.4310, the highest value in its forming column.
- label: Stiffness
benchmark: elastic_modulus
line: Elastic modulus is 193 GPa for annealed material (ATI) and falls to 174 GPa for full-hard material as rolled (ATI).
- label: Heat
benchmark: ultimate_tensile_strength
value: 552 MPa at 204 C
line: Annealed material keeps a typical tensile strength of 552 MPa at 204 C and 401 MPa at 538 C (ATI).
- label: Cold
benchmark: ultimate_tensile_strength
value: 2082 MPa at -196 C, full hard
line: At -196 C full-hard material has a typical tensile strength of 2082 MPa and a yield of 1482 MPa (ATI). The annealed material reaches 1896 MPa at the same temperature.
compare: Compared with the 18-8 grades, ATI says 301's corrosion properties are not as good, and carbide precipitation during welding restricts its use in favour of ATI 304 and 304L. Once work hardened, ATI says 301 develops higher tensile strength than other stable austenitic grades. Outokumpu's strain-hardening exponent of 0.8 is the highest in its forming column.
compare_rows:
- label: Tensile strength, annealed
benchmark: ultimate_tensile_strength
- label: Density
benchmark: density
- label: Melting range
benchmark: melting_point
handling:
- Anneal at 1010 to 1121 C, water-quench heavy sections and air-cool thin ones (ATI).
- After cold rolling, stress-relieve at 371 to 538 C for 5 minutes to 5 hours to make the sheet more isotropic, using the low end of the range to limit carbide precipitation (ATI).
- Weld with 19 9L filler, the welding consumable Outokumpu prints for 1.4310, and plan for carbide precipitation in the heat-affected zone (Outokumpu, ATI).
- Wear protective gloves and use respiratory protection where welding or grinding fumes exceed exposure limits (ATI SDS).
good_for:
- Springs and clips, where cold-work strength is the main requirement (ATI).
- Light formed structures such as truck and trailer bodies, railway and subway cars and aircraft structural parts (ATI, UPMET).
- Bright decorative and trim parts, which ATI describes as having a bright, attractive surface (ATI).
watch_out:
- Welding and holding at 427 to 816 C, which causes carbide precipitation. Outokumpu prints N/N for intergranular corrosion resistance.
- 'Chloride pitting: Outokumpu''s critical pitting temperature is below 10 C in its test, so chloride exposure is the main corrosion risk.'
- Cold work raises magnetic permeability (ATI), so cold-worked parts should not be assumed nonmagnetic.
- Cold-rolled sheet is slightly anisotropic, and the difference is larger in compression (ATI).
verdict: Once work hardened, Type 301 has higher tensile strength than other stable austenitic grades (ATI), but it gives up corrosion resistance and welding ease for that strength. Specify it for springs and light formed structures where cold-work strength is the need, and use 304 or 304L where welding matters.
References
Every number above carries a reference number. Click one to see the source and where in it the value comes from.
| # | Source | Type | Year | Used for |
|---|---|---|---|---|
| ATI 301 Technical Data Sheet, Stainless Steel: Austenitic (UNS S30100), version 1 dated 2/17/2014 | datasheet | 2014 | 66 values | |
| ATI 301 austenitic stainless steel product page (composition, specifications, minimum properties) | datasheet | 0 values | ||
| United Performance Metals: Datasheet for 301 Stainless Steel Sheet and Coil, AMS 5901 (UNS S30100) | datasheet | 2026 | 3 values | |
| Outokumpu: Steel Grades, Properties and Global Standards (Tables 4, 5, 13 and 15) | handbook | 6 values | ||
| ATI Stainless Steel Safety Data Sheet FRP008 (North America, revision date 04-Sep-2018, covers ATI301) | datasheet | 2018 | 5 values | |
| USGS Mineral Commodity Summaries 2026: Nickel | report | 2026 | 2 values | |
| USGS Mineral Commodity Summaries 2026: Chromium | report | 2026 | 2 values | |
| PubChem: Nickel (CID 935), UN GHS classification | database | 1 value | ||
| PubChem: Chromium (CID 23976), UN GHS classification | database | 1 value |