Data still to be completed------(Home) | |
---|---|
PRODUCT DATA of D6AC |
Material | D6AC |
Chemical Composition | Fe-1.1Cr-1Mo-0.6Ni-0.46C |
PHYSICAL PROPERTIES |
---|
Specific Gravity | 7.78 |
ELASTIC PROPERTIES |
---|
Tensile Modulus | 210 GPa |
THERMAL PROPERTIES |
---|
Thermal Expansion Coefficient | 13.3 μstrain/°C |
Specific Heat | 0.486 J/g.K |
Melting Range | 1430 °C |
RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
---|
Stress Corrosion Status | High Resistance to SCC: Table 1: UTS below 1450 MPa Low Resistance to SCC: Table 3: UTS above 1450 MPa UTS Remark: acc. to ECSS-Q-ST-70-36C Data Quality: Design Data |
Machinability | D6AC machines like any of the other low alloy steels. Machining is best done with the alloy in the normalized and tempered condition. Machining, or grinding, of parts that have been heat treated to 200 ksi, or greater, require a 3 hour stress relief anneal after such machining. |
Welding | D6AC may be welded by TIG method for thin sections or by Gas Metal Arc Welding (GMAW) for heavy sections using a filler rod of the same alloy. Care should be used to maintain preheat and interpass weld temperature at 232 to 288 C. Restrained weldments should subsequently be post-heated at 315 C, air cooled to 149 C and then, at once, be stress relieved in a furnace at 538 C followed by re-normalizing and re-tempering. |