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TZM Alloy

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Refractory Metallurgy

Premium Titanium-Zirconium-Molybdenum Refractory Alloy

Sush Tech delivers elite-grade **TZM Alloy**, an advanced solid-solution and particle-strengthened molybdenum-base refractory alloy. It contains microscopic alignments of titanium and zirconium carbides that provide superior recrystallization parameters compared to pure molybdenum configurations.

Engineered to handle extreme thermal stress environments exceeding 1400°C, TZM offers exceptional creep resistance, low thermal expansion coefficients, and superb thermal conductivity boundaries. This makes it an invaluable asset for mission-critical aerospace structures, furnace manufacturing lines, and high-energy engineering distribution channels.

Sush Tech Premium TZM Alloy Profile
Core Advantages

Key Benefits of TZM Refractory Alloy

Elevated Recrystallization

Carbide grain modifications increase the recrystallization temperature threshold to between 1400°C and 1450°C, preventing embrittlement.

Minimal Thermal Expansion

Maintains high dimensional precision and structural boundaries under severe, rapid heating and cooling cycles.

High-Temperature Strength

Carries significantly higher tensile strength parameters at extreme heat bounds compared to unalloyed refractory elements.

Product Applications

Custom Sourced TZM Elements

TZM Alloy High Temperature Furnace Heating Elements

Furnace Structural Parts

High-purity structural shield frames, support rails, and critical charging fixtures built for heavy-duty vacuum processing furnaces.

TZM Alloy Aerospace Rocket Nozzles

Rocket Propulsion Components

Precision-engineered military jet engine gas pipe components and rocket nozzle systems handling highly volatile propellant lines.

TZM Alloy Hot Stamping Dies

Isothermal Forging Dies

Heavy compression forging tool inserts and hot stamping dies designed to shape titanium and superalloy base metals without deforming.

Chemical & Mechanical Specs

TZM Alloy Technical Data Sheet

Alloy Element Breakdown Nominal Composition Weight Percentage (%) Range
Molybdenum (Mo) Balance Profile (Approx. 99.2% – 99.4%)
Titanium (Ti) 0.40% – 0.55% (Sub-micron Carbide Strengthening)
Zirconium (Zr) 0.06% – 0.12% (Grain Boundary Matrix Modification)
Carbon (C) 0.01% – 0.04% (Forming Essential Ti-Zr Interstitial Carbides)
Density Limit Metric 10.22 g/cm³ (Optimal Refractory Configuration Density)