Titanium Grade 5 (Ti-6Al-4V)

UNS R56400

Tensile Strength
≥ 895 MPa (130 ksi)
Yield Strength (0.2%)
≥ 828 MPa (120 ksi)
Elongation
≥ 10%
Hardness
30 – 36 HRC

Overview

The most widely used titanium alloy — accounting for approximately 50% of global titanium consumption. The 6% aluminum and 4% vanadium additions create an alpha-beta alloy with dramatically higher strength than commercially pure grades while retaining excellent corrosion resistance. Heat treatable to even higher strength levels. The standard material for aerospace structures, medical implants, and high-performance marine components.

Chemical Composition (wt%)

ElementMinMax
Ti (Titanium)87.791
Al (Aluminum)5.56.75
V (Vanadium)3.54.5
Fe (Iron)0.4
O (Oxygen)0.2
C (Carbon)0.08
N (Nitrogen)0.05

Mechanical Properties

PropertyValueCondition
Tensile Strength≥ 895 MPa (130 ksi)annealed
Yield Strength (0.2%)≥ 828 MPa (120 ksi)annealed
Elongation≥ 10%annealed
Hardness30 – 36 HRCannealed (330 HB typical)
Density4.43 g/cm³

Physical Properties

PropertyValue
Melting Point1604 – 1660 °C
Thermal Conductivity6.7 W/m·K (at 20°C)
Beta Transus995 °C

Corrosion Resistance

Comparable to Grade 2 in most environments with slightly reduced corrosion resistance in reducing acids due to the vanadium content. Excellent resistance to seawater, chloride solutions, and oxidizing media. Not as formable as Grade 1 or 2 — requires hot working for severe forming operations. The strength-to-corrosion-resistance ratio is unmatched by any other engineering metal.

Typical Applications

Aerospace structural componentsSurgical implants and medical devicesOffshore risers and subsea componentsHigh-performance automotive (connecting rods, valves)Marine propeller shaftsSporting goods (bicycle frames, golf clubs)

Related Standards

ASTM B348ASTM B381AMS 4928AMS 4911ISO 5832-3