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PRODUCT DATA of 4130 |
Material | 4130 |
General Information | AISI 4130 is a low alloy steel containing molybdenum and chromium as strengthening agents |
Processing and Assembly | The alloy can be hardened by heat treatment. |
Chemical Composition | 0.3C-1Cr-0.5Mn-0.2Mo, rem Fe |
EXPERIENCE IN PRACTICE |
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Equivalent Designations | DIN 1.7218, AFNOR 25 CD 4 |
PHYSICAL PROPERTIES |
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Specific Gravity | 7.85 |
ELASTIC PROPERTIES |
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Tensile Modulus | 205 GPa |
Shear Modulus | 50 GPa |
Bulk Modulus | 140 GPa |
Poisson Ratio | 0.27 to 0.3 |
ELECTRICAL PROPERTIES |
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Electrical Volume Resistivity | 2.23e-7 ohm.m |
THERMAL PROPERTIES |
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Thermal Conductivity | 42.7 W/m.K |
Specific Heat | 0.477 J/g.K |
Melting Range | 1430 °C |
RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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General Corrosion Status | Requires specific corrosion protection |
Stress Corrosion Status | High Resistance to SCC: Table 1: UTS below 125 kg/mm2
A small number of laboratory failures of specimens cut from plate more than 2 inches thick have been observed at 75% yield, even within this ultimate strength range. The use of thick plate should therefore be avoided in a corrosive environment when sustained tensile stress in the short transverse direction is expected. Moderate Resistance to SCC: Table 2: UTS 125 to 140 kg/mm2 UTS Remark: Requires Stress corrosion evaluation form Low Resistance to SCC: Table 3: UTS above 140 kg/mm2 UTS Remark: Not for primary structural items Remark: Requires Stress corrosion evaluation form Remark: acc. to ECSS-Q-ST-70-36C Data Quality: Design Data |
Machinability | This alloy is readily machined by conventional methods. Machinability is best with the alloy in the normalized and tempered condition. |