Inconel 706

Verifiedmetal

Inconel 706 is a nickel-iron-based superalloy strengthened by gamma-double-prime precipitation, designed for high-temperature structural applications requiring moderate strength retention to approximately 1300°F (704°C). Primary applications include aircraft engine casings, fasteners, and gas turbine components in aerospace and power generation industries, with excellent creep resistance and thermal fatigue resistance in the intermediate temperature range.

aerospacestructural

Compliance & Regulations

?ITAR?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65

Tempers & Conditions

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Form
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)2 entries
Curve (15 pts)
Pa
Pa22°C · Sheet/Strip/Plate
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
Pa22°C · Sheet/Strip/Plate
Young's Modulus(E)
Pa22°C · Sheet/Strip/Plate
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (25 pts)
1/K
Specific Heat vs Temperature(Cp(T))
Curve (24 pts)
J/(kg·K)
Thermal Conductivity vs Temperature(k(T))
Curve (25 pts)
W/(m·K)
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
kg/m³22°C
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Export Control

Quality & Standards

Industry-Specific

RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.