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Nickel Alloy X-750 SPR-A

Precip hard

UNS N07750 · EN 2.4669 · also Inconel X-750

SPR-A = spring temper + aged

Maximum strength and lowest relaxation — the standard condition for high-temperature springs and clips to ~650 °C.

High cost $$$$

Values for the SPR-A condition

Other X-750 tempers and conditions

X-750 is listed in 8 conditions; see the grade overview at X-750.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest condition for forming, deep drawing and machining before age-hardening.34583045180 HB—
Equalized
Intermediate stabilising treatment used on hot-rolled bar before ageing for bolting and springs.5509003022 HRC1.4 % IACS
Sheet/strip
Formed sheet parts (seals, bellows, diaphragms) aged after forming to reach service strength.7001,1402628 HRC1.4 % IACS
Triple heat treated
Choose for maximum creep-rupture life and notch ductility at 650–815 °C (turbine discs, hot bolting, nuclear internals).7601,1702530 HRC—
STADefault
Solution treated and aged
Standard stocked bar/forging condition: best all-round strength/ductility for bolts, shafts and fasteners to ~700 °C.8151,2002432 HRC—
Equalized + aged
Highest room-temperature strength of the hot-finished bar conditions; typical for high-strength bolting and gas-turbine hardware below 650 °C.8601,2752235 HRC—
No.1 Temper
As-supplied condition for coiling springs; wound cold then precipitation aged by the spring maker.1,2401,450642 HRC1.4 % IACS
SPR-AThis page
Spring temper + aged
Maximum strength and lowest relaxation — the standard condition for high-temperature springs and clips to ~650 °C.1,4501,720546 HRC—

What is X-750 SPR-A?

X-750 SPR-A is X-750 in the SPR-A condition — maximum strength and lowest relaxation — the standard condition for high-temperature springs and clips to ~650 °C. X-750 SPR-A has a yield strength of 1,450 MPa (210 ksi) and a tensile strength of 1,720 MPa (249 ksi) — stronger than 100% of nickel alloy grades. Elongation at break is 5% and the elastic modulus is 214 GPa (31 Msi). X-750 SPR-A has a density of 8.28 g/cm³ (0.299 lb/in³), lighter than 55% of nickel alloy grades. It melts at 1,393°C (2,539 °F). STA is the default condition FabDigit quotes; SPR-A is available on request or by drawing note.

Advantages

  • High strength — 1,450 MPa (210 ksi), better than 100% of nickel alloy grades

Limitations

  • High embodied carbon — 17.5 kg CO₂/kg, worse than 98% of nickel alloy grades
  • Limited ductility — 5%, worse than 93% of nickel alloy grades
  • Difficult to machine — 10/100, worse than 93% of nickel alloy grades
  • Limited formability — 5/100, worse than 91% of nickel alloy grades
  • Difficult to weld — 20/100, worse than 84% of nickel alloy grades

X-750 SPR-A properties

Typical room-temperature values for X-750 SPR-A; 11 are specific to this condition. Other listed values are X-750 reference data and may not represent this condition. Bars are the position among nickel alloy grades.

Physical3

X-750 SPR-A has a density of 8.28 g/cm³ (0.299 lb/in³), lighter than 55% of nickel alloy grades. It melts at 1,393°C (2,539 °F).

Density8.28 g/cm³0.3 lb/in³
Melting Point (Solidus)1,393°C2,539 °F
Liquidus Temperature1,427°C2,601 °F

Mechanical16

X-750 SPR-A has a yield strength of 1,450 MPa (210 ksi) and a tensile strength of 1,720 MPa (249 ksi) — stronger than 100% of nickel alloy grades. Elongation at break is 5% and the elastic modulus is 214 GPa (31 Msi).

Elastic (Young's) Modulus214 GPa31 Msi
Shear Modulus83 GPa12 Msi
Bulk Modulus188 GPa27.3 Msi
Poisson's Ratio0.31
Tensile Strength (Ultimate)1,720 MPa249 ksi
Yield Strength (0.2% offset)1,450 MPa210 ksi
Elongation at Break5%
Reduction in Area35%
Compressive Strength840 MPa122 ksi
Shear Strength1,030 MPa149 ksi
Fatigue Strength (Endurance Limit)600 MPa87 ksi
Fracture Toughness (K_IC)100 MPa·√m91 ksi·√in
Charpy V-Notch Impact (RT)45 J33.2 ft·lbf
Hardness, Brinell440 HB
Hardness, Rockwell C46 HRC
Hardness, Vickers320 HV

Thermal6

X-750 SPR-A is rated for continuous service to 650°C (1,202 °F). It conducts heat at 12 W/m·K (6.93 BTU/hr·ft·°F), better than 65% of nickel alloy grades. Thermal expansion is 12.6 µm/m·K (7 µin/in·°F).

Thermal Conductivity12 W/m·K6.9 BTU/hr·ft·°F
Specific Heat Capacity431 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12.6 µm/m·K7 µin/in·°F
Latent Heat of Fusion290 J/g125 BTU/lb
Max Service Temperature (continuous)650°C1,202 °F
Min Service Temperature-253°C-423 °F

Electrical3

X-750 SPR-A conducts electricity at 1.4 % IACS, worse than 65% of nickel alloy grades.

Electrical Conductivity1.4 % IACS
Electrical Resistivity1.22×10⁻⁶ Ω·m48 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (78/100), better than 51% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.1 V
Corrosion ResistanceVery good78/100
Chemical Resistance SummaryExcellent oxidation and steam resistance to ~980 °C; good in caustics, dilute organic and mineral acids, chloride waters with high resistance to chloride SCC; attacked by hot concentrated HCl/H₂SO₄, oxidising chloride media and sulphidising atmospheres; aged material can be sensitive to hydrogen embrittlement and irradiation-assisted SCC in PWR primary water.

Sustainability4

Producing a kilogram of X-750 SPR-A takes about 290 MJ of energy and emits 17.5 kg of CO₂ — more than 98% of nickel alloy grades. Typical recycled content is 35%.

Embodied Energy (primary production)290 MJ/kg124,678 BTU/lb
Embodied Carbon (primary production)17.5 kg CO₂/kg
Embodied Water300 L/kg35.9 gal/lb
Typical Recycled Content35%

Manufacturability8

X-750 SPR-A's machinability is not recommended (10/100, worse than 93% of nickel alloy grades); weldability poor (20/100); formability not recommended (5/100).

MachinabilityNot recommended10/100
Machinability Rating (AISI 1212 = 100 %)12%
WeldabilityPoor20/100
Formability (cold)Not recommended5/100
CastabilityFair35/100
Brazeability / SolderabilityFair45/100
PolishabilityVery good70/100
Anodizing Responsen/a — nickel alloy; use passivation, electropolish or plating instead

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with X-750 SPR-A

Is X-750 easy to machine?

Machine in the annealed or solution-treated condition where possible; use rigid setups, positive-rake carbide or ceramic tooling, low speed/heavy feed and flood coolant — work hardens rapidly and notches tools like most γ′ superalloys.

Can X-750 be welded?

GTAW/EB weld in the solution-annealed condition with Inconel 69/718-type or matching filler, then re-solution and re-age; welding in the aged condition invites strain-age (post-weld heat-treat) cracking in the HAZ.

Can X-750 be formed, bent or molded?

Cold-form, deep-draw or coil springs in the annealed/spring-temper condition with generous bend radii and frequent interstage anneals; hot work 1150–1230 °C and finish above 950 °C.

What surface finishes work on X-750?

Not anodizable — finish by pickling/passivation, abrasive or electro-polishing; shot peening markedly improves fatigue and SCC life, and silver or dry-film lubricant coatings are used on hot bolting to prevent galling.

X-750 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Cr14 – 1715.5
Fe5 – 97
Ti2.25 – 2.752.5
Al0.4 – 10.7
NbNb + Ta0.7 – 1.20.95
Co≤ 10.3
Mn≤ 10.3
Si≤ 0.50.2
Cu≤ 0.50.1
C≤ 0.080.04
S≤ 0.010
NiNi + Co, balance≥ 70 (balance)—

X-750 SPR-A — frequently asked

What is X-750 SPR-A used for?

X-750 SPR-A is typically used for gas turbine blades and rings, springs, high-temperature bolts and reactor core components. In short: best spring superalloy; low relaxation to 700 °C; hot bolting standard.

What is the yield strength of X-750 SPR-A?

X-750 SPR-A has a typical yield strength of 1,450 MPa (210 ksi) and a tensile strength of 1,720 MPa (249 ksi) — stronger than 100% of nickel alloy grades. Strength varies by condition: see the 8 listed tempers.

Is X-750 SPR-A easy to machine?

Not especially — machinability is rated not recommended (10/100, worse than 93% of nickel alloy grades). Machine in the annealed or solution-treated condition where possible; use rigid setups, positive-rake carbide or ceramic tooling, low speed/heavy feed and flood coolant — work hardens rapidly and notches tools like most γ′ superalloys.

Can X-750 SPR-A be welded?

Not readily — weldability is rated poor (20/100). GTAW/EB weld in the solution-annealed condition with Inconel 69/718-type or matching filler, then re-solution and re-age; welding in the aged condition invites strain-age (post-weld heat-treat) cracking in the HAZ.

What surface finishes work on X-750 SPR-A?

Not anodizable — finish by pickling/passivation, abrasive or electro-polishing; shot peening markedly improves fatigue and SCC life, and silver or dry-film lubricant coatings are used on hot bolting to prevent galling.

Can X-750 SPR-A be formed, bent or molded?

Cold-form, deep-draw or coil springs in the annealed/spring-temper condition with generous bend radii and frequent interstage anneals; hot work 1150–1230 °C and finish above 950 °C.

What is the maximum service temperature of X-750 SPR-A?

X-750 SPR-A is rated for continuous use to about 650°C (1,202 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between X-750-STA and X-750 SPR-A?

STA is the default condition — standard stocked bar/forging condition: best all-round strength/ductility for bolts, shafts and fasteners to ~700 °C. SPR-A: maximum strength and lowest relaxation — the standard condition for high-temperature springs and clips to ~650 °C. Yield strength is 815 MPa in STA versus 1,450 MPa in SPR-A.

Sources

  1. INCONEL alloy X-750 technical bulletin — Special Metals Corporation (2004)
  2. ASTM B637 – Precipitation-Hardening and Cold Worked Nickel Alloy Bars, Forgings and Forging Stock for Moderate or High Temperature Service — ASTM International (2018)
  3. AMS 5667 / AMS 5668 / AMS 5670 / AMS 5698 – Alloy Bars, Wire and Springs, UNS N07750 — SAE International (2019)
  4. AMS 5542 – Nickel Alloy Sheet, Strip and Plate, Solution Heat Treated (UNS N07750) — SAE International (2018)
  5. ASM Handbook Vol.1 – Properties and Selection: Irons, Steels and High-Performance Alloys — ASM International (1990)
  6. ASM Handbook Vol.16 – Machining — ASM International (1989)
  7. High-Temperature Characteristics of Stainless Steels / Nickel Alloy Data — Nickel Institute (2020)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.