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7075-T6 and T62 Clad sheet: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7075 / T6 and T62 / Clad sheet
SpecificationsAMS-QQ-A-250/13
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.6.0, Table 3.7.6.0(c) (pdf page 376 of the chapter file)
Dimension bands5
Density0.101 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 band0.008–0.011 in0.012–0.039 in0.040–0.062 in0.063–0.187 in0.188–0.249 in
SpecificationAMS-QQ-A-250/13AMS-QQ-A-250/13AMS-QQ-A-250/13AMS-QQ-A-250/13AMS-QQ-A-250/13
BasisSABABABAB
Ftu, ksiL…7074717573777577
LT687074717573777577
Fty, ksiL…6265636665696668
LT586063616463676466
Fcy, ksiL…6164626564686567
LT…6467656867716870
Fsu, ksiL…4244424544464546
LT…4244424544464546
Fbru (e/D = 1.5), ksiL…108115110116113119116119
LT…108115110116113119116119
Fbru (e/D = 2.0), ksiL…140148142150146154150154
LT…140148142150146154150154
Fbry (e/D = 1.5), ksiL…90949196941009699
LT…90949196941009699
Fbry (e/D = 2.0), ksiL…105110106112110117112115
LT…105110106112110117112115
e, %L………………………
LT577888888
E, Msi…10.310.310.310.310.310.310.310.3
Ec, Msi…10.510.510.510.510.510.510.510.5
ν…0.330.330.330.330.330.330.330.33
ρ, lb/in3…0.1010.1010.1010.1010.1010.1010.1010.101

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

°FF_tuF_tyF_cyF_suF_bruF_bry
-300117.8117.6
-200110110
-100105.5105.6
0102.9102.8
10098.698.999.899.897.299.5
20089.291.294.79787.596.1
30074.27980.584.677.884.3
40045.75050.558.253.158.5
50019.919.820.227.724.323.1
60011.811.815.614.5

Factors in percent of the room-temperature allowable.

Other 7075 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.