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Stainless Steel AM-355-CRT

Supply condition

UNS S35500 · also Alloy 355, Alloy 634

CRT = 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.

High cost $$$$

Values for the CRT 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—
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
CRTThis page
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-CRT?

AM-355-CRT is AM-355 supplied in the CRT condition — highest-strength strip/spring condition; use for thin flat springs, diaphragms and clamps where forming is done before final ageing. AM-355-CRT has a yield strength of 1,590 MPa (231 ksi) and a tensile strength of 1,720 MPa (249 ksi) — stronger than 100% of stainless steel grades. Elongation at break is 5% and the elastic modulus is 200 GPa (29 Msi). AM-355-CRT 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; CRT is available on request or by drawing note.

Advantages

  • High strength — 1,590 MPa (231 ksi), better than 100% of stainless steel grades

Limitations

  • Limited ductility — 5%, worse than 100% of stainless steel grades
  • Difficult to machine — 15/100, worse than 100% of stainless steel grades
  • Limited formability — 5/100, worse than 99% of stainless steel grades
  • Difficult to weld — 15/100, worse than 98% of stainless steel grades
  • Low fracture toughness — 55 MPa·√m (50.1 ksi·√in), worse than 91% of stainless steel grades

AM-355-CRT properties

Typical room-temperature values for AM-355-CRT; 12 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-CRT 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-CRT has a yield strength of 1,590 MPa (231 ksi) and a tensile strength of 1,720 MPa (249 ksi) — stronger than 100% of stainless steel grades. Elongation at break is 5% 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)1,720 MPa249 ksi
Yield Strength (0.2% offset)1,590 MPa231 ksi
Elongation at Break5%
Reduction in Area50%
Compressive Strength1,100 MPa160 ksi
Shear Strength790 MPa115 ksi
Fatigue Strength (Endurance Limit)720 MPa104 ksi
Fracture Toughness (K_IC)55 MPa·√m50.1 ksi·√in
Charpy V-Notch Impact (RT)22 J16.2 ft·lbf
Hardness, Brinell375 HB
Hardness, Rockwell C48 HRC
Hardness, Vickers490 HV

Thermal6

AM-355-CRT is rated for continuous service to 400°C (752 °F). It conducts heat at 16.3 W/m·K (9.42 BTU/hr·ft·°F), better than 68% of stainless steel grades. Thermal expansion is 11.6 µm/m·K (6.44 µin/in·°F).

Thermal Conductivity16.3 W/m·K9.4 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.6 µm/m·K6.4 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)400°C752 °F
Min Service Temperature-196°C-321 °F

Electrical3

AM-355-CRT 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 fair (52/100), worse than 76% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceFair52/100
Chemical Resistance SummaryResists atmospheric and mildly acidic media better than 410/17-7 PH but below 304; sensitive to chlorides (pitting/SCC) and to strong reducing acids.

Sustainability4

Producing a kilogram of AM-355-CRT 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-CRT's machinability is poor (15/100, worse than 100% of stainless steel grades); weldability poor (15/100); formability not recommended (5/100).

MachinabilityPoor15/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityPoor15/100
Formability (cold)Not recommended5/100
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-CRT

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-CRT — frequently asked

What is AM-355-CRT used for?

AM-355-CRT 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-CRT?

AM-355-CRT has a typical yield strength of 1,590 MPa (231 ksi) and a tensile strength of 1,720 MPa (249 ksi) — stronger than 100% of stainless steel grades. Strength varies by condition: see the 5 listed tempers.

Is AM-355-CRT easy to machine?

Not especially — machinability is rated poor (15/100, worse than 100% 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-CRT be welded?

Not readily — weldability is rated poor (15/100). 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-CRT?

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-CRT 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-CRT?

AM-355-CRT is rated for continuous use to about 400°C (752 °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.