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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.
Carbide grain modifications increase the recrystallization temperature threshold to between 1400°C and 1450°C, preventing embrittlement.
Maintains high dimensional precision and structural boundaries under severe, rapid heating and cooling cycles.
Carries significantly higher tensile strength parameters at extreme heat bounds compared to unalloyed refractory elements.
High-purity structural shield frames, support rails, and critical charging fixtures built for heavy-duty vacuum processing furnaces.
Precision-engineered military jet engine gas pipe components and rocket nozzle systems handling highly volatile propellant lines.
Heavy compression forging tool inserts and hot stamping dies designed to shape titanium and superalloy base metals without deforming.
| 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) |