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PH15-7Mo-TH1050 Sheet, strip, and plate: MIL-HDBK-5J Design Allowables

Material classSteel
Alloy / temper / formPH15-7Mo / TH1050 / Sheet, strip, and plate
SpecificationsAMS 5520
HandbookMIL-HDBK-5J, 31 January 2003, section 2.6.8.0, Table 2.6.8.0(b) (pdf page 184 of the chapter file)
Dimension bands1
Density0.277 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 band0.002–0.500 in
SpecificationAMS 5520
BasisS
Ftu, ksiL185
LT190
Fty, ksiL165
LT170
Fcy, ksiL182
LT188
Fsu, ksiL120
LT120
Fbru (e/D = 1.5), ksiL327
LT327
Fbru (e/D = 2.0), ksiL377
LT377
Fbry (e/D = 1.5), ksiL259
LT259
Fbry (e/D = 2.0), ksiL272
LT272
E, Msi29
Ec, Msi30
G, Msi11.4
ν0.28
ρ, lb/in30.277

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_tyF_cy
10098.498.498.4
20094.194.194.1
300919191
40088.888.888.8
50087.486.186.1
60083.685.185.1
70079.781.581.5
80075.772.672.6

Factors in percent of the room-temperature allowable.

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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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