Tools › Materials › Titanium › Ti-6Al-4V-Alpha-beta processed, annealed Die forging

Ti-6Al-4V-Alpha-beta processed, annealed Die forging: MIL-HDBK-5J Design Allowables

Material classTitanium
Alloy / temper / formTi-6Al-4V / Alpha-beta processed, annealed / Die forging
SpecificationsAMS 4928
HandbookMIL-HDBK-5J, 31 January 2003, section 5.4.1.0, Table 5.4.1.0(f) (pdf page 58 of the chapter file)
Dimension bands3
Density4429 kg/m³

Design Mechanical and Physical Properties (room temperature)

Converted from the handbook table (ksi, Msi, lb/in³) and rounded to 4 significant figures; dimension bands in inches with mm in parentheses. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.

Dimension band0–2 in (0–50.8 mm)2.001–4.000 in (50.83–101.6 mm)4.001–6.000 in (101.6–152.4 mm)
SpecificationAMS 4928AMS 4928AMS 4928
BasisSSS
Ftu, MPaL930.8896.3896.3
LT930.8896.3896.3
ST…896.3896.3
Fty, MPaL861.8827.4827.4
LT861.8827.4827.4
ST…827.4827.4
Fcy, MPaL…848.1848.1
LT…882.5882.5
ST………
Fsu, MPaL…544.7544.7
LT…544.7544.7
ST…544.7544.7
Fbru (e/D = 1.5), MPaL…14001400
LT…14001400
ST…14001400
Fbru (e/D = 2.0), MPaL…17721772
LT…17721772
ST…17721772
Fbry (e/D = 1.5), MPaL…11791179
LT…11791179
ST…11791179
Fbry (e/D = 2.0), MPaL…13861386
LT…13861386
ST…13861386
e, %L101010
LT101010
ST…108
E, GPa116.5116.5116.5
Ec, GPa118.6118.6118.6
G, GPa44.8244.8244.82
ν0.310.310.31
ρ, kg/m³442944294429

Effect of Temperature

Percent of the room-temperature value against temperature, digitized from the handbook figures (the shortest exposure of each figure, every 10 °F). Strength curves give the allowable at temperature; "after exposure" curves give the room-temperature property after a soak at that temperature.

Strength allowables at temperature, percent of room temperature

Moduli at temperature

Elongation and exposure effects

°CF_tuF_tyF_cyF_suF_bruF_bry
-184150.5156.4
-129133135
-73118.1118.8
-18107.5107.6
3898.298.197.497.497.797.7
9390.988.786.79090.287.6
14984.379.477.282.783.278.9
20478.171.169.877.177.771.6
2673.665.26573.173.566
31671.66362.170.971.963.7
37169.66160.268.371.262.1
42766.558.157.965.569.459.8

Factors in percent of the room-temperature allowable.

Other Ti-6Al-4V Tables

Source and Use

U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.