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Ti-4.5Al-3V-2Fe-2Mo-Annealed Sheet: MIL-HDBK-5J Design Allowables

Material classTitanium
Alloy / temper / formTi-4.5Al-3V-2Fe-2Mo / Annealed / Sheet
SpecificationsAMS 4899
HandbookMIL-HDBK-5J, 31 January 2003, section 5.4.3.0, Table 5.4.3.0(b) (pdf page 111 of the chapter file)
Dimension bands2
Density454 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 band0.025–0.063 in (0.635–1.6 mm)0.063–0.187 in (1.6–4.75 mm)
SpecificationAMS 4899AMS 4899
BasisABAB
Ftu, MPaL923.9999.7923.9992.8
LT923.91014923.9992.8
Fty, MPaL868.7923.9868.7910.1
LT868.7944.6868.7923.9
Fcy, MPaL882.5937.7896.3958.4
LT903.2986910.1972.2
Fbru (e/D = 1.5), MPaL1351148214271538
LT1351148214271538
Fbru (e/D = 2.0), MPaL1779195119032041
LT1779195119032041
Fbry (e/D = 1.5), MPaL1082117911381213
LT1082117911381213
Fbry (e/D = 2.0), MPaL1310142713651448
LT1310142713651448
e, %L881010
LT881010
E, GPa110.3110.3110.3110.3
Ec, GPa111.7111.7111.7111.7
ρ, kg/m³4540454045404540

Effect of Temperature

The handbook maps no temperature-effect figure to this table.

Other Ti-4.5Al-3V-2Fe-2Mo 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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.