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Stainless Steel Custom 465-H1100

Precip hard

UNS S46500 · ASTM A564, 5936

H1100 = aged 593 °C (1100 °F) for 4 h

Softer over-aged condition where impact toughness dominates over strength.

CNC machiningSheet metalPremium cost $$$

Values for the H1100 condition

Other Custom 465 tempers and conditions

Custom 465 is listed in 8 conditions; see the grade overview at Custom 465.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
solution annealed (~980 °C, air cooled)
Stock and machining condition — lowest strength, best formability; age after rough machining.7951,0001530 HRC—
Condition A + cold worked
Cold-drawn wire/bar for springs and fasteners; strength rises before aging, aged afterwards for peak properties.1,1401,240838 HRC2.2 % IACS
Overaged 621 °C (1150 °F) for 4 h, maximum toughness
Lowest-strength aged condition; chosen only when maximum ductility/toughness is required.1,1701,2751740 HRC2.3 % IACS
H1100This page
Aged 593 °C (1100 °F) for 4 h
Softer over-aged condition where impact toughness dominates over strength.1,3101,4001643 HRC2.3 % IACS
Aged 4 h at 566 °C (1050 °F), air cool
Over-aged for maximum ductility, toughness and SCC resistance at reduced strength.1,4501,5201545 HRC—
Aged 4 h at 538 °C (1000 °F), air cool
Best strength/toughness balance and the usual choice for fracture-critical and corrosion-exposed parts.1,5501,6551347 HRC—
Aged 4 h at 510 °C (950 °F), air cool
High strength with better toughness than H900 — common for aerospace fasteners and shafts.1,6201,7251249 HRC—
Aged 482 °C (900 °F) for 1 h, peak hardness
Peak-strength condition for maximum tensile/hardness where toughness and SCC margin are secondary.1,6901,7901151 HRC—

What is Custom 465-H1100?

Custom 465-H1100 is Custom 465 in the H1100 condition — softer over-aged condition where impact toughness dominates over strength. Custom 465-H1100 has a yield strength of 1,310 MPa (190 ksi) and a tensile strength of 1,400 MPa (203 ksi) — stronger than 99% of stainless steel grades. Elongation at break is 16% and the elastic modulus is 200 GPa (29 Msi). Custom 465-H1100 has a density of 7.78 g/cm³ (0.281 lb/in³), lighter than 57% of stainless steel grades. It melts at 1,400°C (2,552 °F). Condition A is the default condition FabDigit quotes; H1100 is available on request or by drawing note.

Advantages

  • High strength — 1,310 MPa (190 ksi), better than 99% of stainless steel grades
  • Polishes to a fine finish — 80/100, better than 89% of stainless steel grades

Limitations

  • Limited ductility — 16%, worse than 88% of stainless steel grades
  • Limited formability — 20/100, worse than 86% of stainless steel grades
  • High embodied carbon — 5.6 kg CO₂/kg, worse than 83% of stainless steel grades
  • Difficult to weld — 50/100, worse than 77% of stainless steel grades

Custom 465-H1100 properties

Typical room-temperature values for Custom 465-H1100; 22 are specific to this condition. Other listed values are Custom 465 reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

Custom 465-H1100 has a density of 7.78 g/cm³ (0.281 lb/in³), lighter than 57% of stainless steel grades. It melts at 1,400°C (2,552 °F).

Density7.78 g/cm³0.28 lb/in³
Melting Point (Solidus)1,400°C2,552 °F
Liquidus Temperature1,440°C2,624 °F

Mechanical15

Custom 465-H1100 has a yield strength of 1,310 MPa (190 ksi) and a tensile strength of 1,400 MPa (203 ksi) — stronger than 99% of stainless steel grades. Elongation at break is 16% and the elastic modulus is 200 GPa (29 Msi).

Elastic (Young's) Modulus200 GPa29 Msi
Shear Modulus77 GPa11.2 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,400 MPa203 ksi
Yield Strength (0.2% offset)1,310 MPa190 ksi
Elongation at Break16%
Reduction in Area58%
Compressive Strength1,345 MPa195 ksi
Shear Strength840 MPa122 ksi
Fatigue Strength (Endurance Limit)635 MPa92.1 ksi
Fracture Toughness (K_IC)110 MPa·√m100 ksi·√in
Charpy V-Notch Impact (RT)55 J40.6 ft·lbf
Hardness, Rockwell C43 HRC
Hardness, Vickers423 HV

Thermal5

Custom 465-H1100 is rated for continuous service to 430°C (806 °F). It conducts heat at 17 W/m·K (9.82 BTU/hr·ft·°F), better than 71% of stainless steel grades. Thermal expansion is 10.4 µm/m·K (5.78 µin/in·°F).

Thermal Conductivity17 W/m·K9.8 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)10.4 µm/m·K5.8 µin/in·°F
Max Service Temperature (continuous)430°C806 °F
Min Service Temperature-75°C-103 °F

Electrical2

Custom 465-H1100 has an electrical resistivity of 7.6×10⁻⁷ Ω·m.

Electrical Resistivity7.6×10⁻⁷ Ω·m29.9 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is good (58/100), worse than 62% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceGood58/100
Chemical Resistance SummaryGood resistance to atmospheric corrosion, dilute organics and body fluids; passivates readily. Not suitable for hot chloride, seawater immersion, or reducing acids — pitting and crevice attack occur; peak-aged conditions are the most SCC-sensitive.

Sustainability4

Producing a kilogram of Custom 465-H1100 takes about 85 MJ of energy and emits 5.6 kg of CO₂ — more than 92% of stainless steel grades. Typical recycled content is 35%.

Embodied Energy (primary production)85 MJ/kg36,543 BTU/lb
Embodied Carbon (primary production)5.6 kg CO₂/kg
Embodied Water250 L/kg30 gal/lb
Typical Recycled Content35%

Manufacturability6

Custom 465-H1100's machinability is poor (30/100, worse than 70% of stainless steel grades); weldability fair (50/100); formability poor (20/100).

MachinabilityPoor30/100
Machinability Rating (AISI 1212 = 100 %)28%
WeldabilityFair50/100
Formability (cold)Poor20/100
PolishabilityVery good80/100
Anodizing Responsen/a — stainless steel; use passivation per AMS 2700 / ASTM A967 instead

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

Working with Custom 465-H1100

Is Custom 465 easy to machine?

Rough machine in Condition A with sharp, rigid, positive-rake carbide tooling and heavy flood coolant; finish after aging with low feeds since aged 47–51 HRC material work-hardens and is abrasive due to Ti.

Can Custom 465 be welded?

Good GTAW/EBW/laser weldability with matching or 465 filler, no preheat needed; re-solution-anneal plus age (or at minimum re-age) after welding to restore joint strength.

Can Custom 465 be formed, bent or molded?

Cold form, bend and cold draw only in Condition A; aged material is essentially non-formable, and hot work should be done above ~1000 °C with slow cooling.

What surface finishes work on Custom 465?

Passivate per ASTM A967/AMS 2700 after machining; takes a high mirror polish for surgical use; avoid electroplating in peak-aged tempers or bake for hydrogen embrittlement relief.

Custom 465 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
C≤ 0.020.01
Mn≤ 0.250.1
Si≤ 0.250.1
P≤ 0.02—
S≤ 0.01—
Cr11 – 12.511.75
Ni10.75 – 11.2511
Mo0.75 – 1.251
Tiprimary η-phase strengthener1.5 – 1.81.65
Febalance—

Custom 465-H1100 — frequently asked

What is Custom 465-H1100 used for?

Custom 465-H1100 is typically used for aircraft structural fittings, landing gear components, actuator shafts and rods, high-strength aerospace fasteners, helicopter rotor hardware and drive shafts. In short: premium high-strength PH stainless.

What is the yield strength of Custom 465-H1100?

Custom 465-H1100 has a typical yield strength of 1,310 MPa (190 ksi) and a tensile strength of 1,400 MPa (203 ksi) — stronger than 99% of stainless steel grades. Strength varies by condition: see the 8 listed tempers.

Is Custom 465-H1100 easy to machine?

Not especially — machinability is rated poor (30/100, worse than 70% of stainless steel grades). Rough machine in Condition A with sharp, rigid, positive-rake carbide tooling and heavy flood coolant; finish after aging with low feeds since aged 47–51 HRC material work-hardens and is abrasive due to Ti.

Can Custom 465-H1100 be welded?

With care — weldability is rated fair (50/100). Good GTAW/EBW/laser weldability with matching or 465 filler, no preheat needed; re-solution-anneal plus age (or at minimum re-age) after welding to restore joint strength.

What surface finishes work on Custom 465-H1100?

Passivate per ASTM A967/AMS 2700 after machining; takes a high mirror polish for surgical use; avoid electroplating in peak-aged tempers or bake for hydrogen embrittlement relief.

Can Custom 465-H1100 be formed, bent or molded?

Cold form, bend and cold draw only in Condition A; aged material is essentially non-formable, and hot work should be done above ~1000 °C with slow cooling.

What is the maximum service temperature of Custom 465-H1100?

Custom 465-H1100 is rated for continuous use to about 430°C (806 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between Custom 465 Condition A and Custom 465-H900?

Condition A is the default condition — stock and machining condition — lowest strength, best formability; age after rough machining. H900: peak-strength condition for maximum tensile/hardness where toughness and SCC margin are secondary. Yield strength is 795 MPa in Condition A versus 1,690 MPa in H900.

Can FabDigit make parts in Custom 465-H1100?

Yes — Custom 465-H1100 is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. Custom 465 Stainless Alloy Technical Datasheet — Carpenter Technology (2023)
  2. AMS 5936 — Steel, Corrosion Resistant, Bars/Wire/Forgings (UNS S46500) — SAE International (2021)
  3. ASTM A564/A564M — Hot-Rolled and Cold-Finished Age-Hardening Stainless Steel Bars and Shapes — ASTM (2019)
  4. ASM Handbook Vol. 1 — Properties and Selection: Irons, Steels, and High-Performance Alloys — ASM International (1990)

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.