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Material Specification

Ti-15V-3Cr-3Sn-3Al

Ti-15V-3Cr-3Sn-3Al Fasteners
Metastable Beta Alloy – Cold Formable Strip and Sheet Grade

Titanium 15V-3Cr-3Sn-3Al Fasteners

Buy Titanium 15V-3Cr-3Sn-3Al (Ti-15-3) fasteners, strip components, springs and custom machined parts from Exotic Alloy. Ti-15-3 is a metastable beta alloy carrying nominally 15% vanadium with 3% each of chromium, tin and aluminium, developed specifically as a cold-formable sheet and strip alloy. In the solution-treated condition it can be cold rolled and formed like a stainless steel; aged, it reaches high strength.

Exotic Alloy manufactures Ti-15-3 components to AMS 4914 for sheet, strip and plate and to ASTM B265, in metric M3–M24 and imperial #6–1" sizes, with full EN 10204 3.1 material test certificates for formed sheet metal parts, springs, and cold-headed fastener applications.

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Product Range

Ti-15V-3Cr-3Sn-3Al Fasteners Available

Ti-15V-3Cr-3Sn-3Al Hex Bolts
Ti-15V-3Cr-3Sn-3Al
Hex Bolts
Ti-15V-3Cr-3Sn-3Al Heavy Hex Bolts
Ti-15V-3Cr-3Sn-3Al
Heavy Hex Bolts
Ti-15V-3Cr-3Sn-3Al Stud Bolts
Ti-15V-3Cr-3Sn-3Al
Stud Bolts
Ti-15V-3Cr-3Sn-3Al Threaded Rods
Ti-15V-3Cr-3Sn-3Al
Threaded Rods
Ti-15V-3Cr-3Sn-3Al Anchor Bolts
Ti-15V-3Cr-3Sn-3Al
Anchor Bolts
Ti-15V-3Cr-3Sn-3Al Hex Nuts
Ti-15V-3Cr-3Sn-3Al
Hex Nuts
Ti-15V-3Cr-3Sn-3Al Washers
Ti-15V-3Cr-3Sn-3Al
Washers
Ti-15V-3Cr-3Sn-3Al Cotter Pins
Ti-15V-3Cr-3Sn-3Al
Cotter Pins
Ti-15V-3Cr-3Sn-3Al Springs
Ti-15V-3Cr-3Sn-3Al
Springs
Ti-15V-3Cr-3Sn-3Al Circlips
Ti-15V-3Cr-3Sn-3Al
Circlips
Ti-15V-3Cr-3Sn-3Al Coated Fasteners
Ti-15V-3Cr-3Sn-3Al
Coated Fasteners
Ti-15V-3Cr-3Sn-3Al Custom Spacers
Ti-15V-3Cr-3Sn-3Al
Custom Spacers
Technical Data

Ti-15V-3Cr-3Sn-3Al Specifications

Chemical Composition — Titanium 15V-3Cr-3Sn-3Al (wt. %)
ElementTiVCrSnAlOFeC
Min %Balance14.002.502.502.50–––
Max %Balance16.003.503.503.500.130.250.05
Mechanical Properties — Titanium 15V-3Cr-3Sn-3Al
ConditionUTS (MPa)YS 0.2% (MPa)Elongation (%)Hardness
Solution Treated (Typical)790–900760–86015–22–
Solution Treated & Aged (Typical)1000–1240965–11706–10–
Condition for Cold Forming–––Solution treated, unaged
Alloy Class–––Metastable beta
Physical Properties
DensityApproximately 4.76 g/cm³
Modulus of ElasticityApproximately 83–103 GPa depending on condition
Melting RangeApproximately 1482–1593°C
Thermal ConductivityApproximately 8.1 W/m·K at 20°C
Maximum Service TemperatureApproximately 315°C
Alloy ClassMetastable beta — cold formable then age hardened
Equivalent Grades & Standards
UNSWerkstoff / DINASTM DesignationCommon Name
R58153 – AMS 4914 / ASTM B265 Ti-15-3 / Ti-15V-3Cr-3Sn-3Al

Key Specifications: AMS 4914 (Sheet, Strip & Plate) / ASTM B265. The UNS designation for this alloy is reported inconsistently — the producer lists R58153, while R58010 and R58150 also appear in circulation. Order against the alloy name and the AMS specification, and confirm the UNS on the certificate. 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. Machine in the solution-treated condition where possible and finish after ageing. Much of this alloy moves as thin strip and foil rather than machined bar, and for those forms stamping, coining and forming practice governs.

Welding: fusion welding of load-bearing joints is not recommended for a metastable beta alloy. 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. Mechanical fastening is the intended joining route.

Forming: this is the whole point of the alloy. In the solution-treated condition Ti-15-3 is soft and ductile enough to be cold rolled to thin strip and foil and cold formed into complex shapes — behaviour no alpha-beta titanium alloy of comparable final strength offers. Form, head or thread roll first, then age.

Heat Treatment: solution treat to retain the metastable beta phase, cold work or form, then age to precipitate alpha and develop strength. The ageing cycle sets the final strength level and should be stated on the order. 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-15-3 was developed to be formed, and that is why it is specified. The metastable beta structure in the solution-treated condition gives cold formability comparable to an austenitic stainless steel, so sheet can be rolled thin, drawn and formed into shapes that would be impossible in Ti-6Al-4V, and fasteners can be cold headed and thread rolled before ageing. The subsequent age then develops 1000 to 1240 MPa typical strength in the finished shape.

For a fastener that route produces a better part than machining hard material: the rolled thread carries continuous grain flow and a cold-worked surface, with the fatigue performance that follows. The trade-offs are a density on the high side for titanium at around 4.76 g/cm³, a modest service ceiling near 315°C, and corrosion behaviour that follows the alloyed rather than the commercially pure grades.

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.

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

  • Developed specifically as a cold-formable sheet and strip alloy.
  • Cold formability comparable to austenitic stainless when solution treated.
  • Ages to 1000–1240 MPa typical after forming.
  • Suits cold heading and thread rolling before ageing.
  • Available as thin strip and foil as well as bar.

Typical Applications

  • Formed sheet metal components requiring high final strength.
  • Springs, clips and spring-temper components.
  • Cold-headed and thread-rolled fasteners.
  • Aerospace sheet metal structure.
  • Thin strip and foil applications.