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Ti-10V-2Fe-3Al-Solution treated and aged (900-950 F) Conventional die forging: MIL-HDBK-5J Design Allowables

Material classTitanium
Alloy / temper / formTi-10V-2Fe-3Al / Solution treated and aged (900-950 F) / Conventional die forging
SpecificationsAMS 4983; AMS 4984
HandbookMIL-HDBK-5J, 31 January 2003, section 5.5.3.0, Table 5.5.3.0(b) (pdf page 141 of the chapter file)
Dimension bands2
Density0.168 lb/in3

Design Mechanical and Physical Properties (room temperature)

As printed in the handbook table. 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 band0–1 in0–3 in
SpecificationAMS 4983AMS 4984
BasisSS
Ftu, ksiL180173
LT180173
ST…173
Fty, ksiL160160
LT160160
ST…160
Fcy, ksiL168168
LT166166
ST…166
Fsu, ksiL10197
LT10197
ST…97
Fbru (e/D = 1.5), ksiL244234
LT244234
ST…234
Fbru (e/D = 2.0), ksiL295284
LT295284
ST…284
Fbry (e/D = 1.5), ksiL227227
LT227227
ST…227
Fbry (e/D = 2.0), ksiL261261
LT261261
ST…261
e, %L44
LT44
ST…4
E, Msi15.915.9
Ec, Msi16.316.3
ρ, lb/in30.1680.168

Effect of Temperature

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

Other Ti-10V-2Fe-3Al 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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.