NICKEL-COPPER ALLOY — AGE-HARDENABLE

Monel K500 Tube Sheet

Monel 400's chemistry with aluminum and titanium added for age-hardening — roughly three times the yield strength of standard 400, for services that need Monel's corrosion resistance and can't accept 400's relatively low strength.

UNS N05500 ASTM B865 Precipitation-hardened

Chemical Composition

ElementMin %Max %
Nickel (Ni)63.070.0
Copper (Cu)27.033.0
Aluminum (Al)2.303.15
Titanium (Ti)0.350.85

Mechanical Properties (Age-Hardened)

PropertyTypical Value
Tensile Strength1050 MPa (aged condition)
Yield Strength (0.2% offset)750 MPa (aged condition)
Elongation20% min
Max. Practical Service Temp.~425°C (strength-limited)

Equivalent Grades

StandardDesignation
ASTM / UNSN05500
EN / DIN2.4375
Trade NameMonel® K-500 (Special Metals)

K500 vs. 400 — Which One

Attribute
Monel 400
Monel K500
Yield Strength
170-280 MPa
~750 MPa (aged)
Heat Treatment
Annealed only
Requires age-hardening
Best For
General HF/seawater service
Where higher strength is also required

See the full Monel 400 datasheet for the standard annealed grade.

Applications

High-strength fasteners and components in the same seawater and sour-service environments as Monel 400, where the added strength allows thinner sections or higher mechanical loading — pump shafts and valve trim are more common than tube sheets, but the alloy is specified where both corrosion resistance and strength are required together.

Advantages & Limitations

Advantages

  • ~3x the yield strength of standard Monel 400
  • Retains Monel's corrosion resistance profile
  • Good resistance to seawater and sour service

Limitations

  • Requires precipitation-hardening heat treatment after machining
  • Higher cost and longer lead time than Monel 400
  • Lower practical temperature ceiling than the annealed grade

FAQ

Usually not — most tube sheet applications are governed by pressure/thickness calculations that standard Monel 400 satisfies without needing K500's extra strength. K500 is reserved for cases with a specific mechanical loading requirement beyond typical pressure-boundary duty.

The corrosion resistance mechanism is largely unaffected by the aging heat treatment, since it comes from the base nickel-copper chemistry rather than the aluminum/titanium precipitates that provide strength.

Yes, particularly in the aged condition — machining is typically done before aging where possible, since the material is softer and easier to work with before the strengthening heat treatment is applied.

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