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Material Specification

Ti-8Al-1Mo-1V

Ti-8Al-1Mo-1V Fasteners
Near-Alpha Titanium Alloy – Highest Stiffness, Service to 455°C

Titanium 8Al-1Mo-1V Fasteners

Buy Titanium 8Al-1Mo-1V (Ti-811 / legacy Grade 8 / UNS R54810) bolts, studs, machined components and forgings from Exotic Alloy. Ti-8Al-1Mo-1V is a near-alpha alloy carrying 7.35 to 8.35% aluminium with about 1% each of molybdenum and vanadium. Its high aluminium content gives it the highest elastic modulus and the lowest density of the common titanium alloys, with useful service to around 455°C.

Exotic Alloy manufactures Ti-8Al-1Mo-1V components to the governing AMS and MIL-T-9046 and MIL-T-9047 specifications in metric M6–M36 and imperial ¼"–1½" sizes, with full EN 10204 3.1 material test certificates for aero-engine fan and compressor hardware and airframe structure where stiffness rather than raw strength governs the design.

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Product Range

Ti-8Al-1Mo-1V Fasteners Available

Ti-8Al-1Mo-1V Hex Bolts
Ti-8Al-1Mo-1V
Hex Bolts
Ti-8Al-1Mo-1V Heavy Hex Bolts
Ti-8Al-1Mo-1V
Heavy Hex Bolts
Ti-8Al-1Mo-1V Stud Bolts
Ti-8Al-1Mo-1V
Stud Bolts
Ti-8Al-1Mo-1V Threaded Rods
Ti-8Al-1Mo-1V
Threaded Rods
Ti-8Al-1Mo-1V Anchor Bolts
Ti-8Al-1Mo-1V
Anchor Bolts
Ti-8Al-1Mo-1V Hex Nuts
Ti-8Al-1Mo-1V
Hex Nuts
Ti-8Al-1Mo-1V Washers
Ti-8Al-1Mo-1V
Washers
Ti-8Al-1Mo-1V Cotter Pins
Ti-8Al-1Mo-1V
Cotter Pins
Ti-8Al-1Mo-1V Springs
Ti-8Al-1Mo-1V
Springs
Ti-8Al-1Mo-1V Circlips
Ti-8Al-1Mo-1V
Circlips
Ti-8Al-1Mo-1V Coated Fasteners
Ti-8Al-1Mo-1V
Coated Fasteners
Ti-8Al-1Mo-1V Custom Spacers
Ti-8Al-1Mo-1V
Custom Spacers
Technical Data

Ti-8Al-1Mo-1V Specifications

Chemical Composition — Titanium 8Al-1Mo-1V (wt. %)
ElementTiAlMoVOFeNC
Min %Balance7.350.750.75––––
Max %Balance8.351.251.250.120.300.050.08
Mechanical Properties — Titanium 8Al-1Mo-1V
ConditionUTS (MPa)YS 0.2% (MPa)Elongation (%)Hardness
Duplex Annealed (Typical)100095015–
Solution Treated & Aged (Typical)1070–1170980–107010–15–
Maximum Service Temperature–––Approximately 455°C
Alloy Class–––Near-alpha
Physical Properties
DensityApproximately 4.37 g/cm³ — lowest of the common Ti alloys
Modulus of ElasticityApproximately 124 GPa — highest of the common Ti alloys
Melting RangeApproximately 1538–1649°C
Thermal ConductivityApproximately 6.5 W/m·K at 20°C
Maximum Service TemperatureApproximately 455°C
Alloy ClassNear-alpha — creep resistant, weldable, not deeply hardenable
Equivalent Grades & Standards
UNSWerkstoff / DINASTM DesignationCommon Name
R54810 – AMS / MIL-T-9046 and 9047 Ti-811 / legacy Grade 8

Key Specifications: SAE AMS and MIL-T-9046 and MIL-T-9047 specifications by product form. Not covered by ASTM B348. A caution on specification numbers. This alloy is covered by SAE AMS and MIL specifications rather than by ASTM B348, and the AMS numbers quoted for it differ between published sources — partly because several have been revised or superseded over the years. Acceptance values must come from the current SAE revision or the customer drawing that governs your parts, not from a catalogue listing. Our certified test values for your actual product form and heat treatment are supplied with every batch.

Machinability: titanium’s low thermal conductivity is the governing problem — the heat generated at the cut stays at the cutting edge instead of being carried away. Use rigid setups, sharp tooling, low surface speeds, heavy positive feeds and high-volume flood coolant directed into the cutting zone, and never let the tool dwell. Fine chips and grinding dust are a fire hazard and are handled wet. Threads are rolled rather than cut wherever the section permits, both for fatigue life and because cutting titanium threads invites the same galling that affects them in service. The high aluminium content makes Ti-811 harder and more abrasive than Ti-6Al-4V and its thermal conductivity is lower still, so surface speeds come down accordingly.

Welding: as a near-alpha alloy Ti-811 is weldable — better than the alpha-beta and beta alloys — which together with its creep resistance is the reason it exists. Welding requires full inert gas shielding of the weld, the heat-affected zone and the root — trailing shields and backing gas are standard practice. Weld colour is the first-pass check: bright silver is acceptable, straw and blue indicate increasing contamination, and grey or white powder means the weld must be cut out. Post-weld stress relief is normally applied.

Forming: hot work in the 900–1010°C range. Cold formability is poor; the high aluminium content makes the alloy stiff and relatively unforgiving, and most forming is done hot.

Heat Treatment: the usual condition is duplex annealed. A solution treatment and age raises strength modestly, but near-alpha alloys are not deeply hardenable in the way the beta alloys are — the strength comes mainly from the aluminium in solid solution. All heat treatment above roughly 500°C must be carried out in vacuum or inert gas, or the oxygen-enriched alpha case removed afterwards, because titanium absorbs oxygen, nitrogen and hydrogen rapidly at temperature and a contaminated surface layer is brittle.

Ti-8Al-1Mo-1V is chosen for stiffness and creep resistance, not corrosion performance, and its high aluminium content brings a specific liability that buyers must know about. Titanium alloys with aluminium above roughly 6% are susceptible to stress corrosion cracking in hot salt and, notably, in methanol and some other alcohols — Ti-811 at 7.35 to 8.35% aluminium sits at the high end of that range and is the most susceptible of the alloys on this page. It should not be used in methanol-bearing service or in hot salt deposit conditions under sustained tensile stress without specific qualification.

For general corrosion duty the commercially pure and lean grades are the correct choice; Ti-811 earns its place where a component must be stiff, light and creep resistant at up to 455°C.

Titanium alloys divide into four classes, and the class tells you more than the grade number does. Alpha and near-alpha alloys are weldable and creep resistant and run hottest, but are not heat treatable to high strength. Alpha-beta alloys — of which Ti-6Al-4V is the archetype — are heat treatable, strong and the general structural choice. Near-beta and metastable beta alloys are deeply hardenable, can be cold formed in the solution-treated condition and then aged to very high strength, which makes them the natural choice for fasteners and springs. Commercially pure and lean corrosion grades trade all strength away for corrosion performance.

A note on the grade number. This alloy is widely referred to by a grade number, but that number is a historical designation and does not appear in the current ASTM B265 or B348 grade lists — those run 1 to 7, then 9, then 11 to 21, 23 and upward, skipping 8 and 10. Ordering against the bare grade number alone is therefore risky; order against the UNS number and the AMS or MIL specification, and confirm the product form.

Three absolute exclusions apply to every titanium grade: it must not be used in dry chlorine, with which it reacts violently; not with red fuming nitric acid; and it is rapidly attacked by hydrofluoric acid at any concentration. Fine titanium swarf and grinding dust are a fire hazard and are handled wet.

Titanium galls, and for a threaded fastener this is the dominant practical issue. A titanium thread run against another titanium thread will cold-weld and seize, often badly enough that the fastener has to be cut off. Every titanium bolted joint needs one of three mitigations: an anti-seize compound or dry-film lubricant such as molybdenum disulphide; a plated or coated thread, commonly silver or solid-film lubricant; or a nut in a dissimilar material. Specify which at order stage.

Titanium is galvanically noble. It will not corrode itself, but a titanium fastener in an aluminium, carbon steel, zinc or magnesium assembly drives accelerated corrosion of the structure around it, and a bolted joint’s small-anode, large-cathode geometry is the worst case. Insulating washers and sleeves or a barrier coating should be specified in those assemblies.

Key Characteristics

  • Highest elastic modulus of the common titanium alloys at around 124 GPa.
  • Lowest density of the common titanium alloys at around 4.37 g/cm³.
  • Near-alpha structure gives good weldability and creep resistance.
  • Useful service to approximately 455°C.
  • Specific stiffness higher than Ti-6Al-4V, which is why it is specified.

Typical Applications

  • Aero engines: fan and compressor blade and disc hardware.
  • Airframe structure where stiffness governs over strength.
  • Elevated-temperature fastener assemblies to 455°C.
  • Engine casings and static hot-section components.
  • Weight and stiffness critical aerospace fixings.