TaMo

metal
· JVASP-127515· TaMo

TaMo is a refractory metal alloy combining tantalum and molybdenum, designed to maintain strength and resist oxidation at extremely high temperatures where conventional metals fail. This material is primarily used in demanding aerospace and industrial applications requiring exceptional thermal stability, such as rocket engine components, furnace linings, and high-temperature structural elements. Engineers select TaMo when operating temperatures exceed the capabilities of nickel-based superalloys, though its brittle nature at lower temperatures and high cost typically limit its use to critical, temperature-critical applications rather than general structural use.

rocket engine nozzleshigh-temperature furnace componentsrefractory structural partsaerospace thermal protectionrefractory crucibles

Compliance & Regulations

?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
PropertyValueUnitConditionsSource
Density(ρ)
13.68
kg/m³
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Band Gap(Eg)
0.000
eV
Magnetic Moment(μB)
0.000
µB
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Energy Above Hull(ΔEhull)
0.000800
eV/atom
Formation Energy(ΔHf)
-0.2020
eV/atom
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Export Control

RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.