Technical Reference Library
Ti-8Al-1Mo-1V Titanium Alloy
UNS R54810
AMS 4915
Alloy Type Near-Alpha
Material Overview
Ti-8Al-1Mo-1V is a near-alpha titanium alloy defined by its unusually high 8% aluminum content, paired with small, roughly equal additions of molybdenum and vanadium that provide just enough beta-phase stabilization to aid processing without turning the alloy into a true alpha-beta grade. That heavy alpha-side loading gives the alloy the lowest density of any commercially significant titanium alloy, along with good strength and creep resistance that hold up well at elevated service temperatures.
That combination of low weight and elevated-temperature strength retention is what makes Ti-8Al-1Mo-1V a long-standing choice for jet engine compressor sections — forged compressor blades and discs in particular, where every gram of rotating mass matters and the material has to keep its strength through sustained thermal cycling. It's a purpose-built alloy for that specific role rather than a general-purpose titanium grade.
International Designation Equivalents
| Standard |
Designation |
| UNS |
R54810 |
| AMS |
4915 (sheet, strip, plate) |
| AMS |
4972 (bar, wire, ring) |
Chemical Composition
| Element |
Content |
| Aluminum (Al) |
7.35 – 8.35% |
| Molybdenum (Mo) |
0.75 – 1.25% |
| Vanadium (V) |
0.75 – 1.25% |
| Iron (Fe) |
0.30% max |
| Oxygen (O) |
0.15% max |
| Carbon (C) |
0.08% max |
| Nitrogen (N) |
0.05% max |
| Hydrogen (H) |
0.0125% max |
| Titanium (Ti) |
Balance |
Machinability Explained
Ti-8Al-1Mo-1V carries the same core titanium machining challenges as any other grade — low thermal conductivity that concentrates heat at the tool edge, a reactive surface that promotes tool wear at elevated cutting temperature, and a tendency to work-harden under a rubbing or dull edge. Where it differs from a heavily beta-stabilized alloy is in the relatively small amount of beta phase present, which tends to make near-alpha grades like this one somewhat more forgiving to cut than the higher-vanadium alpha-beta grades in the same family.
Its very low density also works in the machinist's favor to some degree, since removal rates and cutting forces for a given depth of cut tend to run a bit lighter than on denser titanium alloys. That said, the high aluminum content still promotes chemical reactivity with tool materials at cutting temperature, so the same fundamentals apply: moderate speeds, firm and consistent feeds to stay under any hardened surface layer, rigid setups, and generous coolant flow directed right at the cutting zone.
Overall, this alloy tends to machine somewhat more predictably than the higher-strength alpha-beta titanium grades, though it still demands the discipline any titanium alloy requires — sharp tooling, adequate feed, and no dwelling in the cut.
Recommended Cutting Speeds
| Operation |
Vc (m/min) |
Vc (SFM) |
| Turning |
65 – 85 |
215 – 280 |
| Milling |
45 – 65 |
150 – 215 |
| Parting |
40 – 55 |
130 – 180 |
| Grooving |
55 – 75 |
180 – 245 |
| Drilling |
55 – 75 |
180 – 245 |
Values assume favorable cutting conditions: a well-matched insert grade, maximum rigidity in tool and workpiece clamping, good-quality raw material, short tool overhang, and flood coolant. Reduce further for interrupted cuts, thin-wall sections, or reduced rigidity.
Recommended FM Carbide Grades by Operation
Turning
| Grade |
Coating |
ISO Application Range |
| FM524 |
CVD |
S05 – S10 |
| FM2533 |
CVD |
S15 |
Parting Off
| Grade |
Coating |
ISO Application Range |
| FM2543 |
CVD |
S20 |
| FM2553 |
CVD |
S30 |
Grooving
| Grade |
Coating |
ISO Application Range |
| FM2533 |
CVD |
S10 |
Milling (Indexable)
| Grade |
Coating |
ISO Application Range |
| FM125 |
PVD |
S15 – S35 |
Recommended Insert Cutting-Edge Geometry
| Parameter |
Value |
| Honing Size |
0.02 – 0.05 mm / 0.001 – 0.002" |
| Rake Angle |
13° – 18° |
| Land Angle |
Neutral |
| Land Width |
0.10 – 0.20 mm / 0.004 – 0.008" |
| Ground Insert |
Recommended |