NICKEL-CHROMIUM HIGH-TEMPERATURE ALLOY

Alloy 602 CA

Alloy 602 CA is a high-carbon nickel-chromium alloy engineered for exceptional creep strength and oxidation resistance at very high temperatures. Aluminium, carbon, titanium, zirconium and yttrium contribute to its high-temperature performance.

UNS N06025 NAME 602 CA SPEC Product specification / manufacturer certification required
MATERIAL OVERVIEW

Alloy 602 CA Information

Alloy 602 CA is a high-carbon nickel-chromium alloy engineered for exceptional creep strength and oxidation resistance at very high temperatures. Aluminium, carbon, titanium, zirconium and yttrium contribute to its high-temperature performance.

Metallic winding and compatible ring components where service conditions are suitable.

UNS Number N06025
Common Name 602 CA
Material Type Ni-Cr-Fe-Al-C high-temperature alloy
Common / Applicable Specification Product specification / manufacturer certification required
Typical Gasket Use Metallic winding and compatible ring components where service conditions are suitable.
CHEMICAL PROPERTIES

Alloy 602 CA Chemical Composition

Reference composition limits are shown below. Exact requirements should be confirmed against the applicable product specification and certified material documentation.

Element / Constituent Symbol Composition / Information
Nickel Ni Balance
Chromium Cr 24.0–26.0
Iron Fe 8.0–11.0
Aluminium Al 1.8–2.4
Carbon C 0.15–0.25
Titanium Ti 0.10–0.20
Zirconium Zr 0.01–0.12
Yttrium Y 0.05–0.12
Manganese Mn 0.15 max.
Silicon Si 0.50 max.
MECHANICAL PROPERTIES

Alloy 602 CA Mechanical Properties

Reference room-temperature properties are shown for a commonly supplied condition. Exact requirements depend on product form, size, heat treatment and governing specification.

Property Reference Value Unit / Basis
Tensile Strength Typical ≈680–750 MPa
0.2% Offset Yield Strength Typical ≈270–350 MPa
Elongation Typical ≈30–40 %

Values shown are engineering reference data, not universal design allowables. Final procurement and design must use the governing specification, exact product form/condition and certified material test documentation.

ENGINEERING INFORMATION

Alloy 602 CA Physical & Service Information

Reference physical properties and service considerations relevant to material selection for Spiral Wound Gaskets.

Density Approx. 7.9 g/cm³
Structure Austenitic nickel-base alloy
High-Temperature Behaviour Excellent creep and oxidation resistance in very high-temperature service.
Heat Treatment Typically solution annealed.
Service Selection Mechanical values are strongly product- and condition-dependent; use certified supplier data for design.
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