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Stainless Steel AM-355 SCT1000

Precip hard

UNS S35500 · also Alloy 355, Alloy 634

Slightly lower strength than SCT 850 but better ductility, toughness and stress-corrosion behaviour; preferred for thick sections and higher service temperature.

High cost $$$$

Values for the SCT1000 condition

Other AM-355 tempers and conditions

AM-355 is listed in 5 conditions; see the grade overview at AM-355.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution annealed
Supply condition for forming, machining and welding before the customer runs the SCT hardening cycle.4501,0002525 HRC—
SCT1000This page
equalized, sub-zero cooled and tempered at 540 °C
Slightly lower strength than SCT 850 but better ductility, toughness and stress-corrosion behaviour; preferred for thick sections and higher service temperature.1,0001,1701937 HRC2.2 % IACS
Double aged
Simplified hardening route for sheet and welded assemblies where sub-zero cooling is impractical; strength somewhat below SCT 850.1,0301,2401239 HRC2.2 % IACS
SCT850Default
equalized, sub-zero cooled and tempered at 455 °C
Peak-strength aerospace condition — choose when maximum tensile/fatigue strength is the driver and toughness demands are moderate.1,0701,2751740 HRC2.2 % IACS
Cold rolled (Condition A strip) and tempered/aged
Highest-strength strip/spring condition; use for thin flat springs, diaphragms and clamps where forming is done before final ageing.1,5901,720548 HRC—

What is AM-355 SCT1000?

AM-355 SCT1000 is AM-355 in the SCT1000 condition — slightly lower strength than SCT 850 but better ductility, toughness and stress-corrosion behaviour; preferred for thick sections and higher service temperature. AM-355 SCT1000 has a yield strength of 1,000 MPa (145 ksi) and a tensile strength of 1,170 MPa (170 ksi) — stronger than 98% of stainless steel grades. Elongation at break is 19% and the elastic modulus is 200 GPa (29 Msi). AM-355 SCT1000 has a density of 7.91 g/cm³ (0.286 lb/in³), heavier than 76% of stainless steel grades. It melts at 1,400°C (2,552 °F). SCT850 is the default condition FabDigit quotes; SCT1000 is available on request or by drawing note.

Advantages

  • High strength — 1,000 MPa (145 ksi), better than 98% of stainless steel grades

Limitations

  • Limited formability — 12/100, worse than 93% of stainless steel grades
  • Difficult to machine — 25/100, worse than 88% of stainless steel grades
  • Difficult to weld — 35/100, worse than 86% of stainless steel grades
  • Low fracture toughness — 70 MPa·√m (63.7 ksi·√in), worse than 83% of stainless steel grades
  • Limited ductility — 19%, worse than 81% of stainless steel grades

AM-355 SCT1000 properties

Typical room-temperature values for AM-355 SCT1000; 37 are specific to this condition. Other listed values are AM-355 reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

AM-355 SCT1000 has a density of 7.91 g/cm³ (0.286 lb/in³), heavier than 76% of stainless steel grades. It melts at 1,400°C (2,552 °F).

Density7.91 g/cm³0.29 lb/in³
Melting Point (Solidus)1,400°C2,552 °F
Liquidus Temperature1,450°C2,642 °F

Mechanical16

AM-355 SCT1000 has a yield strength of 1,000 MPa (145 ksi) and a tensile strength of 1,170 MPa (170 ksi) — stronger than 98% of stainless steel grades. Elongation at break is 19% 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)1,170 MPa170 ksi
Yield Strength (0.2% offset)1,000 MPa145 ksi
Elongation at Break19%
Reduction in Area55%
Compressive Strength1,030 MPa149 ksi
Shear Strength730 MPa106 ksi
Fatigue Strength (Endurance Limit)585 MPa84.8 ksi
Fracture Toughness (K_IC)70 MPa·√m63.7 ksi·√in
Charpy V-Notch Impact (RT)34 J25.1 ft·lbf
Hardness, Brinell345 HB
Hardness, Rockwell C37 HRC
Hardness, Vickers365 HV

Thermal6

AM-355 SCT1000 is rated for continuous service to 480°C (896 °F). It conducts heat at 16.5 W/m·K (9.53 BTU/hr·ft·°F), better than 70% of stainless steel grades. Thermal expansion is 11.8 µm/m·K (6.56 µin/in·°F).

Thermal Conductivity16.5 W/m·K9.5 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.8 µm/m·K6.6 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)480°C896 °F
Min Service Temperature-196°C-321 °F

Electrical3

AM-355 SCT1000 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)-0.15 V
Corrosion ResistanceGood57/100
Chemical Resistance SummaryGood resistance to atmosphere, steam and mild acids; the higher temper improves resistance to chloride stress-corrosion cracking relative to the 455 °C temper.

Sustainability4

Producing a kilogram of AM-355 SCT1000 takes about 57 MJ of energy and emits 4.6 kg of CO₂ — more than 62% of stainless steel grades. Typical recycled content is 40%.

Embodied Energy (primary production)57 MJ/kg24,506 BTU/lb
Embodied Carbon (primary production)4.6 kg CO₂/kg
Embodied Water150 L/kg18 gal/lb
Typical Recycled Content40%

Manufacturability8

AM-355 SCT1000's machinability is poor (25/100, worse than 88% of stainless steel grades); weldability fair (35/100); formability not recommended (12/100).

MachinabilityPoor25/100
Machinability Rating (AISI 1212 = 100 %)23%
WeldabilityFair35/100
Formability (cold)Not recommended12/100
CastabilityPoor25/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100
Anodizing Responsen/a — ferrous alloy; use passivation (AMS 2700), electropolish or plating instead of anodizing.

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

Working with AM-355 SCT1000

Is AM-355 easy to machine?

Machine in Condition A wherever possible; in SCT 850 use rigid setups, positive-rake carbide or ceramic, heavy feeds and low speeds to cut under the work-hardened layer, with flood coolant.

Can AM-355 be welded?

GTAW/GMAW/EB weld in Condition A with matching or AM-355 filler, low heat input and no preheat, then run the full equalize–refrigerate–temper cycle to restore joint strength; welding after hardening is not recommended.

Can AM-355 be formed, bent or molded?

Cold form only in Condition A (austenitic, work-hardens rapidly — allow generous bend radii and interstage annealing); hot forge 1150–950 °C followed by re-annealing.

What surface finishes work on AM-355?

Passivate per AMS 2700/ASTM A967 after machining; electropolishing and fine mechanical polishing work well, and shot peening is common to raise fatigue life in hardened parts.

AM-355 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
Chigher than AM-350 (0.07–0.11) — the main strength difference0.1 – 0.150.13
Mn0.5 – 1.250.9
Si≤ 0.50.3
P≤ 0.04—
S≤ 0.03—
Cr15 – 1615.5
Ni4 – 54.5
Mo2.5 – 3.252.9
Naustenite stabiliser controlling the transformation response0.07 – 0.130.1
Febalance—

AM-355 SCT1000 — frequently asked

What is AM-355 SCT1000 used for?

AM-355 SCT1000 is typically used for aircraft forgings, structural fittings and fasteners. In short: stronger than AM-350; forging-grade PH stainless; 40 HRC after SCT.

What is the yield strength of AM-355 SCT1000?

AM-355 SCT1000 has a typical yield strength of 1,000 MPa (145 ksi) and a tensile strength of 1,170 MPa (170 ksi) — stronger than 98% of stainless steel grades. Strength varies by condition: see the 5 listed tempers.

Is AM-355 SCT1000 easy to machine?

Not especially — machinability is rated poor (25/100, worse than 88% of stainless steel grades). Machine in Condition A wherever possible; in SCT 850 use rigid setups, positive-rake carbide or ceramic, heavy feeds and low speeds to cut under the work-hardened layer, with flood coolant.

Can AM-355 SCT1000 be welded?

With care — weldability is rated fair (35/100). GTAW/GMAW/EB weld in Condition A with matching or AM-355 filler, low heat input and no preheat, then run the full equalize–refrigerate–temper cycle to restore joint strength; welding after hardening is not recommended.

What surface finishes work on AM-355 SCT1000?

Passivate per AMS 2700/ASTM A967 after machining; electropolishing and fine mechanical polishing work well, and shot peening is common to raise fatigue life in hardened parts.

Can AM-355 SCT1000 be formed, bent or molded?

Cold form only in Condition A (austenitic, work-hardens rapidly — allow generous bend radii and interstage annealing); hot forge 1150–950 °C followed by re-annealing.

What is the maximum service temperature of AM-355 SCT1000?

AM-355 SCT1000 is rated for continuous use to about 480°C (896 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between AM-355 SCT850 and AM-355-A?

SCT850 is the default condition — peak-strength aerospace condition — choose when maximum tensile/fatigue strength is the driver and toughness demands are moderate. A: supply condition for forming, machining and welding before the customer runs the SCT hardening cycle. Yield strength is 1,070 MPa in SCT850 versus 450 MPa in A.

Sources

  1. ASTM A564/A564M — Hot-Rolled and Cold-Finished Age-Hardening Stainless Bars and Shapes (Type 355 / UNS S35500) — ASTM International (2019)
  2. AMS 5743 — Steel, Corrosion Resistant, Bars and Forgings, 15.5Cr–4.5Ni–2.9Mo, Consumable Electrode Melted, SCT — SAE International (2018)
  3. AMS 5547 — Steel, Corrosion Resistant, Sheet, Strip and Plate, 15.5Cr–4.5Ni–2.9Mo (AM-355) — SAE International (2017)
  4. ASM Handbook Vol. 1 — Properties and Selection: Irons, Steels and High-Performance Alloys (semi-austenitic PH stainless) — ASM International (1990)
  5. MMPDS-16 — Metallic Materials Properties Development and Standardization, AM-355 sections — Battelle/FAA (2021)
  6. ASM Handbook Vol. 13B — Corrosion: Materials — ASM International (2005)

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.