Buy Titanium 6Al-6V-2Sn (Ti-662 / UNS R56620) bolts, studs, machined components and forgings from Exotic Alloy. Ti-662 is a highly beta-stabilised two-phase alpha-beta alloy, modified from the Ti-6Al-4V system by raising vanadium to 5–6% and adding tin, copper and iron. The result is appreciably higher strength and better deep hardenability than Ti-6Al-4V, at some cost in ductility and weldability.
Exotic Alloy manufactures Ti-662 components to the governing AMS specifications — including AMS 4971 and AMS 4978 for bar and forgings and AMS 4918 for plate, sheet and strip — and to MIL-T-9046 and MIL-T-9047, in metric M6–M36 and imperial ¼"–1½" sizes, with full EN 10204 3.1 material test certificates for airframe structure and ordnance components.
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| Element | Ti | Al | V | Sn | Cu | Fe | O | C |
|---|---|---|---|---|---|---|---|---|
| Min % | Balance | 5.00 | 5.00 | 1.50 | 0.35 | 0.35 | – | – |
| Max % | Balance | 6.00 | 6.00 | 2.50 | 1.00 | 1.00 | 0.20 | 0.05 |
| Condition | UTS (MPa) | YS 0.2% (MPa) | Elongation (%) | Hardness |
|---|---|---|---|---|
| Annealed (Typical) | 1035–1105 | 965–1035 | 10–14 | – |
| Solution Treated & Aged (Typical) | 1170–1275 | 1100–1200 | 8–10 | – |
| Strength Relative to Ti-6Al-4V | Approximately 15% higher | – | Lower ductility | – |
| Alloy Class | – | – | – | Alpha-beta, highly beta stabilised |
| Density | Approximately 4.54 g/cm³ |
| Modulus of Elasticity | Approximately 110 GPa |
| Melting Range | Approximately 1538–1649°C |
| Thermal Conductivity | Approximately 6.6 W/m·K at 20°C |
| Maximum Service Temperature | Approximately 315°C |
| Alloy Class | Alpha-beta — deeply hardenable, limited weldability |
| UNS | Werkstoff / DIN | ASTM Designation | Common Name |
|---|---|---|---|
| R56620 | – | AMS 4918 / 4971 / 4978 / MIL-T-9046 and 9047 | Ti-662 / Ti-6-6-2 |
Key Specifications: AMS 4971 and AMS 4978 (Bar & Forgings) / AMS 4918 (Plate, Sheet & Strip) / MIL-T-9046 and MIL-T-9047. 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B348, and the AMS numbers quoted for it differ between published sources — partly because several have been revised or superseded over the years.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.