Application center
Titanium and nickel powder selection guidance for lightweight structures, hot-side components, propulsion support, and flight hardware.
Specifications & quotation
Use these as candidate routes, not automatic approvals. The quotation confirms source, grade, PSD, evidence scope, quantity, and delivery terms.
A widely used titanium alloy powder for lightweight structural AM parts where strength-to-weight performance matters.
Near-alpha titanium powder for elevated-temperature structural programs and aerospace development work.
Precipitation-hardenable nickel alloy powder for high-temperature structures, turbines, and energy hardware.
Oxidation-resistant nickel alloy powder for combustion, furnace, hot-gas, and high-temperature hardware.
Where Ti64 powder makes sense for aerospace structural AM parts, with attention to weight-driven geometry, process fit, and qualification-sensitive applications.
Select CuCrZr or C18150 powder for a regeneratively cooled rocket chamber liner, including alloy boundaries, cooling channels, bimetallic jackets, inspection, and RFQ fields.
Select IN718, IN625, Alloy X, or a program-specific nickel alloy powder for rocket chamber jackets, preburners, manifolds, nozzles, and hot-fire hardware.
Compare IN718, IN625, Alloy X, Ti64, and copper-alloy powder routes for rocket injectors, cryogenic valves, feed manifolds, and RFQs.
Where IN718 powder can fit gas turbine fuel nozzle bodies, combustor swirler hardware, injector-adjacent supports, and LPBF hot-section flow parts.
Send grade, particle size, quantity and destination. Paid samples from 1 kg; export licence and dangerous-goods shipping handled. Exporting metal powders since 2016.