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Stainless Steel 17-6PH-H950

Precip hard

AISI/SAE 17-6PH · UNS S17600 · also Alloy 635

H950 = aged 510 °C (950 °F) / 1–4 h, air cool

High-strength aerospace condition for fasteners, shafts and spring elements with acceptable ductility.

High cost $$$$

Values for the H950 condition

Other 17-6PH tempers and conditions

17-6PH is listed in 7 conditions; see the grade overview at 17-6PH.

Compare all 7 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
ADefault
Solution annealed
Stock/supply condition: machine, form and cold-head here, then age in one step with minimal distortion.7609651230 HRC—
Aged 593 °C (1100 °F) for 4 h
Maximum-ductility overaged condition for weldments and parts needing best SCC resistance at ~1000 MPa.9001,0351533 HRC—
Aged 565 °C (1050 °F) / 4 h, air cool
Overaged, toughest useful strength level — choose for thick sections, impact loading or chloride-bearing service.1,0351,1401337 HRC—
Cold drawn, Condition A
Cold-drawn spring wire supplied for coiling and subsequent single-step age hardening.1,0701,240640 HRC2.1 % IACS
Aged 540 °C (1000 °F) / 4 h, air cool
Balanced condition: ~1240 MPa with better toughness and stress-corrosion margin than H950.1,1401,2401141 HRC—
H950This page
Aged 510 °C (950 °F) / 1–4 h, air cool
High-strength aerospace condition for fasteners, shafts and spring elements with acceptable ductility.1,2401,345944 HRC—
Aged 482 °C (900 °F) for 1 h, peak hardness
Peak-strength aging for springs and small fasteners where hardness matters more than toughness or SCC margin.1,2751,380845 HRC—

What is 17-6PH-H950?

17-6PH-H950 is 17-6PH in the H950 condition — high-strength aerospace condition for fasteners, shafts and spring elements with acceptable ductility. 17-6PH-H950 has a yield strength of 1,240 MPa (180 ksi) and a tensile strength of 1,345 MPa (195 ksi) — stronger than 99% of stainless steel grades. Elongation at break is 9% and the elastic modulus is 200 GPa (29 Msi). 17-6PH-H950 has a density of 7.8 g/cm³ (0.282 lb/in³), heavier than 50% of stainless steel grades. It melts at 1,400°C (2,552 °F). A is the default condition FabDigit quotes; H950 is available on request or by drawing note.

Advantages

  • High strength — 1,240 MPa (180 ksi), better than 99% of stainless steel grades

Limitations

  • Limited ductility — 9%, worse than 99% of stainless steel grades
  • Difficult to machine — 24/100, worse than 93% of stainless steel grades
  • Limited formability — 12/100, worse than 93% of stainless steel grades
  • Difficult to weld — 30/100, worse than 88% of stainless steel grades
  • Limited service temperature — 315°C (599 °F), worse than 85% of stainless steel grades

17-6PH-H950 properties

Typical room-temperature values for 17-6PH-H950; 17 are specific to this condition. Other listed values are 17-6PH reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

17-6PH-H950 has a density of 7.8 g/cm³ (0.282 lb/in³), heavier than 50% of stainless steel grades. It melts at 1,400°C (2,552 °F).

Density7.8 g/cm³0.28 lb/in³
Melting Point (Solidus)1,400°C2,552 °F
Liquidus Temperature1,450°C2,642 °F

Mechanical14

17-6PH-H950 has a yield strength of 1,240 MPa (180 ksi) and a tensile strength of 1,345 MPa (195 ksi) — stronger than 99% of stainless steel grades. Elongation at break is 9% 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 Ratio0.28
Tensile Strength (Ultimate)1,345 MPa195 ksi
Yield Strength (0.2% offset)1,240 MPa180 ksi
Elongation at Break9%
Reduction in Area33%
Shear Strength800 MPa116 ksi
Fatigue Strength (Endurance Limit)610 MPa88.5 ksi
Charpy V-Notch Impact (RT)18 J13.3 ft·lbf
Hardness, Brinell285 HB
Hardness, Rockwell C44 HRC
Hardness, Vickers435 HV

Thermal6

17-6PH-H950 is rated for continuous service to 315°C (599 °F). It conducts heat at 16 W/m·K (9.24 BTU/hr·ft·°F), better than 58% of stainless steel grades. Thermal expansion is 10.8 µm/m·K (6 µin/in·°F).

Thermal Conductivity16 W/m·K9.2 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)10.8 µm/m·K6 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)315°C599 °F
Min Service Temperature-75°C-103 °F

Electrical3

17-6PH-H950 conducts electricity at 2.2 % IACS, worse than 61% of stainless steel grades.

Electrical Conductivity2.2 % IACS
Electrical Resistivity8×10⁻⁷ Ω·m31.5 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is good (57/100), worse than 66% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.25 V
Corrosion ResistanceGood57/100
Chemical Resistance SummaryGood resistance to atmospheric, mild chloride and dilute organic acid exposure — roughly equal to 17-4PH and clearly better than 410; not suitable for hot chlorides, reducing acids (HCl, H2SO4) or seawater immersion, and susceptible to hydrogen embrittlement / SCC when aged below 540 °C.

Sustainability4

Producing a kilogram of 17-6PH-H950 takes about 56 MJ of energy and emits 5 kg of CO₂ — more than 59% of stainless steel grades. Typical recycled content is 35%.

Embodied Energy (primary production)56 MJ/kg24,076 BTU/lb
Embodied Carbon (primary production)5 kg CO₂/kg
Embodied Water210 L/kg25.2 gal/lb
Typical Recycled Content35%

Manufacturability7

17-6PH-H950's machinability is poor (24/100, worse than 93% of stainless steel grades); weldability poor (30/100); formability not recommended (12/100).

MachinabilityPoor24/100
Machinability Rating (AISI 1212 = 100 %)24%
WeldabilityPoor30/100
Formability (cold)Not recommended12/100
Brazeability / SolderabilityFair45/100
PolishabilityVery good75/100
Anodizing Responsen/a — stainless steel is not anodized; use passivation per ASTM A967 or electropolishing

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

Working with 17-6PH-H950

Is 17-6PH easy to machine?

Machine in Condition A with rigid setups, sharp positive-rake carbide, heavy positive feeds and flood coolant; the alloy work-hardens quickly, so avoid dwelling and expect ~40 % of 1212 rates (drop to ~25 % after H950 aging).

Can 17-6PH be welded?

GTAW/GMAW/EBW with matching or 17-4PH filler is possible, but the Ti-bearing weld metal loses much of its aging response — post-weld solution treat plus re-age wherever full properties are required.

Can 17-6PH be formed, bent or molded?

Cold form, bend, coil or cold-head only in Condition A; aging causes very little distortion or size change, so form to near-net shape first and age last.

What surface finishes work on 17-6PH?

Passivate per ASTM A967 (nitric or citric) after machining; electropolishing improves pitting resistance, and shot peening after aging restores fatigue life — plate only with baking at 190 °C to avoid hydrogen embrittlement.

17-6PH 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≤ 0.080.06
Mn≤ 10.5
Si≤ 10.5
P≤ 0.04—
S≤ 0.03—
Cr16 – 17.516.75
Ni6 – 7.56.8
Tiprimary age-hardening element (Ni3Ti)0.4 – 1.20.75
Al≤ 0.40.2
Febalance—

17-6PH-H950 — frequently asked

What is 17-6PH-H950 used for?

17-6PH-H950 is typically used for springs, fasteners and aerospace structural clips. In short: forms soft, ages hard; low distortion on aging; limited mill availability.

What is the yield strength of 17-6PH-H950?

17-6PH-H950 has a typical yield strength of 1,240 MPa (180 ksi) and a tensile strength of 1,345 MPa (195 ksi) — stronger than 99% of stainless steel grades. Strength varies by condition: see the 7 listed tempers.

Is 17-6PH-H950 easy to machine?

Not especially — machinability is rated poor (24/100, worse than 93% of stainless steel grades). Machine in Condition A with rigid setups, sharp positive-rake carbide, heavy positive feeds and flood coolant; the alloy work-hardens quickly, so avoid dwelling and expect ~40 % of 1212 rates (drop to ~25 % after H950 aging).

Can 17-6PH-H950 be welded?

Not readily — weldability is rated poor (30/100). GTAW/GMAW/EBW with matching or 17-4PH filler is possible, but the Ti-bearing weld metal loses much of its aging response — post-weld solution treat plus re-age wherever full properties are required.

What surface finishes work on 17-6PH-H950?

Passivate per ASTM A967 (nitric or citric) after machining; electropolishing improves pitting resistance, and shot peening after aging restores fatigue life — plate only with baking at 190 °C to avoid hydrogen embrittlement.

Can 17-6PH-H950 be formed, bent or molded?

Cold form, bend, coil or cold-head only in Condition A; aging causes very little distortion or size change, so form to near-net shape first and age last.

What is the maximum service temperature of 17-6PH-H950?

17-6PH-H950 is rated for continuous use to about 315°C (599 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 17-6PH-A and 17-6PH-H900?

A is the default condition — stock/supply condition: machine, form and cold-head here, then age in one step with minimal distortion. H900: peak-strength aging for springs and small fasteners where hardness matters more than toughness or SCC margin. Yield strength is 760 MPa in A versus 1,275 MPa in H900.

Sources

  1. ASM Handbook Vol. 1: Properties and Selection — Irons, Steels and High-Performance Alloys (precipitation-hardening stainless steels) — ASM International (1990)
  2. SAE AMS 5638 / UNS S17600 — Stainless W (Type 635) chemistry and heat treatment — SAE International (2018)
  3. ASM Handbook Vol. 13B: Corrosion — Materials (stainless steel corrosion behaviour) — ASM International (2005)
  4. ASTM A967 — Chemical Passivation Treatments for Stainless Steel Parts — ASTM International (2017)
  5. MMPDS-style typical room-temperature property tables for PH stainless steels — Battelle / FAA (2023)

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.