Refractory Alloys Molybdenum - Titanium Alloy

Not applicable.

Anneal in protective atmosphere at 2400 to 2600 F. Stress relief anneal at 2000 to 2200 F in protective atmosphere for one hour.

Used for aerospace applications such as heat shields.

May be cold worked by conventional methods.

Good corrosion resistance to many acids, except hydrofluoric acid. Good in reducing atmospheres, but will oxidize in air at elevated temperatures.

No data.

The alloy may be bent, shaped or formed by conventional means.

Not applicable.

Not applicable.

No data.

Machinable by conventional methods.

This is a molybdenum alloy containing 0.5% titanium.

Not applicable.

May be fusion or resistance welded. Note that at temperatures above 900 f the alloy will rapidly oxidize in air.