• Monel Alloy K-500/UNS N05500/W.Nr. 2.4375
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Monel Alloy K-500/UNS N05500/W.Nr. 2.4375

Monel Alloy K-500/UNS N05500/W.Nr. 2.4375
Phone:+8617768786989
Email:simon@alloysfactory.com
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◉ PRODUCT SPECIFICATION

Monel Alloy K‑500 (UNS N05500) builds on Monel 400 by including approximately 2.3–3.15% aluminum and 0.35–0.85% titanium. This addition, along with age-hardening treatment, results in a precipitation of Ni₃(Ti, Al) phases, delivering notably higher strength while retaining corrosion resistance.

Specifications & Parameters

CategoryPropertyValue / SpecificationCondition / Notes
Chemical CompositionNickel (Ni)63.0–70.0%Base element

Copper (Cu)27.0–33.0%Primary alloying element

Aluminum (Al)2.3–3.15%Precipitation hardening element

Titanium (Ti)0.35–0.85%

Iron (Fe)≤2.0%

Manganese (Mn)≤1.5%

Carbon (C)≤0.25%

Silicon (Si)≤0.50%

Sulfur (S)≤0.01%
Physical PropertiesDensity8.44–8.80 g/cm³ (0.305–0.318 lb/in³)

Melting Range1300–1350°C (2372–2462°F)

Electrical Resistivity51–62 μΩ·cmAt 20°C

Thermal Conductivity17.5–22.0 W/m·KAt 100°C

Coefficient of Thermal Expansion (20–100°C)13.4–13.9 × 10⁻⁶/°C

Elastic Modulus179–214 GPa (26,000–31,000 ksi)

Magnetic Permeability<1.005 (Non-magnetic below −101°C/−150°F)
Mechanical PropertiesTensile Strength690–1310 MPa (100–190 ksi)Varies by product form/condition

Yield Strength (0.2% Offset)276–827 MPa (40–120 ksi)

Elongation (A5)15–45%

Hardness172–413 HB (Brinell)
35–40 HRC (Rockwell C)
Precipitation-hardened state
Thermal PropertiesContinuous Service Limit (Air)≤650°C (1202°F)Oxidation resistance

Stress Rupture Strength (600°C/1,000h)~40 MPa (5.8 ksi)
Corrosion ResistanceSeawaterExcellent (resists pitting/SCC in flowing seawater; risk in stagnant water)

Hydrofluoric Acid (HF)Exceptional resistanceSuperior to most alloys

Alkalis & Organic AcidsHighly resistant

Chloride Stress Corrosion Cracking (SCC)Near-immunity
Heat TreatmentSolution Annealing870–980°C (1600–1800°F), rapid coolOptimizes ductility

Precipitation Hardening480–650°C (900–1200°F), 4–16h holdEnhances strength via γ' phase (Ni₃(Al,Ti))
FabricationWeldingTIG/MIG with ERNiCu-7 filler
Must be done in annealed state; stress-relieve before aging


MachinabilityChallenging (high work-hardening; requires carbide tools/low speeds)
International StandardsBar/RodASTM B164, AMS 7234Aerospace grade

Plate/SheetASTM B127, AMS 4553

Tubing/PipeASTM B165, AMS 4676

ForgingsASTM B564
Key ApplicationsMarine EngineeringPump shafts, propeller blades, seawater valves, fasteners

Oil & GasDrill collars, valve stems, downhole tools (NACE MR0175 compliant)

AerospaceTurbine blades, springs, high-strength bolts

Chemical ProcessingHF acid equipment, reactor components, scrubbers

? Critical Notes & Variability Factors

  1. Mechanical Property Ranges:

    • Strength/ductility vary significantly with product form (bar, sheet, wire) and heat treatment (annealed vs. aged). Aerospace grades (e.g., AMS 4676) require higher minimum strengths.

    • Cold working further increases strength but reduces elongation.

  2. Corrosion Limitations:

    • Avoid strong oxidizers (e.g., nitric acid) and stagnant seawater (risk of pitting).

    • Susceptible to stress corrosion cracking in hot HF vapor under high stress.

  3. Thermal Stability:

    • Prolonged exposure above 550°C (1022°F) may cause embrittlement; limit to 480°C (900°F) for critical applications.

  4. Nuclear/Aerospace Compliance:

    • Special grades (e.g., ASTM B164 for nuclear) enforce stricter controls on Al/Ti ratios and impurities.

? Summary: Monel® K-500 combines the corrosion resistance of Monel® 400 with doubled tensile strength via γ' precipitation hardening. Its niche dominance in marine, oil/gas, and aerospace stems from unparalleled HF/seawater resistance, non-magnetic behavior, and reliability up to 650°C. For project-specific validation, consult ASTM/AMS standards directly.

global price comparison

FormChina (Local suppliers)Europe (UK/EU)USA (Local suppliers)India (Local suppliers)
Plate/Sheet$20–38 /kg FOB; $28–40 /kg FOB (various listings)£28/kg (~$36)₹3,500–4,500/kg (~$45–58)
Bar/Rod$15–20 /kg (bar)£20–28/kg (~US$24–34)$20–50 /kg₹1,600–2,000/kg (~$24–30)
Coil/Strip$30–48 /kg£24–30/kg ($30–37)₹3,000–3,500/kg (~$40–45) (≈₹3k typical)
Wire$30–60 /kg; spring/welding wire $35–45/kg (10–499 kg)£23–30/kg ($29–37)$30–45 /kg₹3,600–4,500/kg (~$48–60)

? Key Insights

  • China offers the most competitive K‑500 pricing globally, especially for wire and coil.

  • Europe/UK prices hover between $30–$37/kg depending on form.

  • USA distributor quotes for bar/rod are broad, ranging $20–50/kg.

  • India pricing is higher—₹1,600–4,500/kg ($24–$60/kg)—depending on form and certification.

? Note: Prices can vary depending on MOQ, certification, surface finish, and currency fluctuations.

Why MWalloys Chooses K‑500

  • Strength & Hardness: Offers higher tensile strength vs Monel 400 (e.g., ~1,100 MPa aged).

  • Exceptional Corrosion Resistance: Maintains Monel 400’s resistance even in sour-gas and seawater, though aged K‑500 may be more prone to SCC in some niches.

  • Cryo Temperature Performance: Excellent toughness without brittle transition down to –210 °C.

Manufacturing & Forming

Alloy K‑500 can be hot- or cold-worked. Typical age-hardening: solution annealing (~980–1,050 °C), quenching, followed by aging (~480–540 °C). Proper heat-treating avoids TiC formation and optimizes mechanical properties.

Comparison with Monel 400 & Other Alloys

FeatureK‑500Monel 400Inconel 718 (Ni-superalloy)
Tensile Strength (RT)~1,100 MPa~620 MPa~1,100 MPa
Corrosion ResistanceExcellent, with SCC caution agedExcellent, marine-gradeVery Good
Age-HardenableYesNoYes (γ′/γ″ precipitates)
MagneticNon-magneticNon-magneticNon-magnetic

Welding Best Practices

Use compatible Ni-Cu filler, preheat as needed, stress-relieve, then age-harden post-weld to recover full strength.

FAQS

1. Why choose Monel K‑500 over Monel 400?

Despite having corrosion resistance similar to Monel 400, Monel K‑500 incorporates aluminum and titanium, which enable precipitation hardening—significantly boosting strength and hardness to 1,100 MPa in aged conditions. It remains tough even at cryogenic (–210 °C) or elevated temperatures.

2. How well does K‑500 resist corrosion – especially in sour or marine conditions?

K‑500 maintains similarly low corrosion rates as Monel 400 in both high-velocity seawater and hydrogen sulfide environments. However, aged K‑500 shows a slightly higher tendency for stress-corrosion cracking, so its use requires proper material processing.

3. What’s the recommended heat cycle for welding to regain full strength?

To prevent post-weld strain-age cracking, K‑500 should be welded in the solution-annealed condition, followed by a stress relief, and then re-aged (e.g., 900–1,000 °F) to restore mechanical properties via gamma prime precipitates.

4. Which welding processes and fillers are ideal for K‑500?

The best approach is gas-tungsten arc welding (GTAW/TIG) with ERNiCu‑7 (Monel 60); you can also use covered electrodes like AWS ENiCrMo‑3 for SMAW. Ensure weld edges are oxide-free, inter-pass temperature stays below 120 °C, and post-weld brushing occurs before aging.

5. How does K‑500 perform at low temperatures and under fatigue?

K‑500 remains highly ductile even down to –423 °F, without a ductile-to-brittle transition. It also retains excellent fatigue strength—aging and cold working boost fatigue resistance by over 30%—making it ideal for springs, shafts, and cyclic loads.



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