HAYNES HR-120 Annealed

Verifiedmetal

HAYNES HR-120 is a nickel-iron-chromium superalloy designed for high-temperature structural applications requiring intermediate strength and excellent oxidation resistance up to approximately 1200°F (649°C). The annealed condition provides optimized ductility and toughness for forming and fabrication while maintaining adequate yield strength, making it suitable for aerospace engine components, ducting, and thermal protection systems per AMS 5916.

aerospacestructural

Compliance & Regulations

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

HAYNES HR-120/HAYNES HR-120 Annealed

Units:

si imperial

Property OverviewNormalized to typical max values

3 interactive curves for this material

Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.

Create free account

Filter by

Form

Thickness

Basis

Orientation

Property	Value	Unit	Conditions
Elongation at Break(εf)2 entries	30.00	-	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=>0.015 to 0.749 in
↳	30.00	-	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=0.750 to 2.000 in
Ultimate Tensile Strength(σUTS)4 entries	90.00	ksi	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=>0.015 to 0.749 in
↳	101	ksi	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=>0.015 to 0.749 in
↳	90.00	ksi	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=0.750 to 2.000 in
↳	Curve (21 pts)	ksi	L
Yield Strength (0.2% offset)(σy)4 entries	40.00	ksi	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=>0.015 to 0.749 in
↳	44.00	ksi	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=>0.015 to 0.749 in
↳	40.00	ksi	22°C · Sheet/Strip/Plate · Annealed · AMS 5916 · LT · t=0.750 to 2.000 in
↳	Curve (21 pts)	ksi	L
Young's Modulus vs Temperature(E(T))	Curve (19 pts)	ksi	—

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, or test environment.

Rows with are inherited from the base material

Verified Unverified Low confidence (<80%) Link to source

3 interactive curves for this material

Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.

Create free account

Property	Value	Unit	Conditions
CTE vs Temperature(α(T))	Curve (9 pts)	µin/in·°F	—
Specific Heat vs Temperature(Cp(T))	Curve (12 pts)	BTU/(lb·°F)	—
Thermal Conductivity vs Temperature(k(T))	Curve (12 pts)	BTU/(hr·ft·°F)	—

Verified Unverified Low confidence (<80%) Link to source

Property	Value	Unit	Conditions	Source
Density(ρ)	0.3240	lb/in³	22°C

Rows with are inherited from the base material

Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Export Control

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.

HAYNES HR-120 Annealed

Mechanical Properties

Thermal Properties

Physical Properties

Regulatory Screening

Environmental

Export Control