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Ti-6Al-2Sn-4Zr-2Mo-Triplex annealed Sheet: MIL-HDBK-5J Design Allowables

Material classTitanium
Alloy / temper / formTi-6Al-2Sn-4Zr-2Mo / Triplex annealed / Sheet
SpecificationsAMS-T-9046, Comp. AB-4
HandbookMIL-HDBK-5J, 31 January 2003, section 5.3.3.0, Table 5.3.3.0(b) (pdf page 45 of the chapter file)
Dimension bands1
Density0.164 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 band0.000–0.187 in
SpecificationAMS-T-9046, Comp. AB-4
BasisS
Ftu, ksiL145
LT145
Fty, ksiL135
LT135
E, Msi16.5
Ec, Msi18
G, Msi6.2
ρ, lb/in30.164

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

°FF_tuF_ty
10097.697.6
20092.289.5
30086.882.3
40082.375.5
50078.369.8
60075.365.3
70073.862.6
80060.8

Factors in percent of the room-temperature allowable.

Other Ti-6Al-2Sn-4Zr-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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.