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7075-T6, T651, and T62 Bar, rod, and shapes: rolled, drawn, or cold-finished: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7075 / T6, T651, and T62 / Bar, rod, and shapes: rolled, drawn, or cold-finished
SpecificationsAMS 4122, AMS 4123, AMS 4186, AMS 4187, and AMS-QQ-A-225/9
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.6.0, Table 3.7.6.0(d) (pdf page 380 of the chapter file)
Dimension bands4
Density2796 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 band0–1 in (0–25.4 mm)1.001–2.000 in (25.43–50.8 mm)2.001–3.000 in (50.83–76.2 mm)3.001–4.000 in (76.23–101.6 mm)
SpecificationAMS 4122, AMS 4123, AMS 4186, AMS 4187, and AMS-QQ-A-225/9AMS 4122, AMS 4123, AMS 4186, AMS 4187, and AMS-QQ-A-225/9AMS 4122, AMS 4123, AMS 4186, AMS 4187, and AMS-QQ-A-225/9AMS 4122, AMS 4123, AMS 4186, AMS 4187, and AMS-QQ-A-225/9
BasisABABABAB
Ftu, MPaL530.9544.7530.9544.7530.9544.7530.9544.7
LT530.9544.7517.1530.9496.4510.2475.7489.5
Fty, MPaL455.1468.8455.1468.8455.1468.8455.1468.8
LT455.1468.8455.1468.8434.4448.2413.7427.5
Fcy, MPaL441.3455.1441.3455.1441.3455.1441.3455.1
LT……………………
Fsu, MPaL317.2324.1317.2324.1317.2324.1317.2324.1
LT317.2324.1317.2324.1317.2324.1317.2324.1
Fbru (e/D = 1.5), MPaL689.5710.2689.5710.2689.5710.2689.5710.2
LT689.5710.2689.5710.2689.5710.2689.5710.2
Fbru (e/D = 2.0), MPaL848.1868.7848.1868.7848.1868.7848.1868.7
LT848.1868.7848.1868.7848.1868.7848.1868.7
Fbry (e/D = 1.5), MPaL592.9606.7592.9606.7592.9606.7592.9606.7
LT592.9606.7592.9606.7592.9606.7592.9606.7
Fbry (e/D = 2.0), MPaL634.3655634.3655634.3655634.3655
LT634.3655634.3655634.3655634.3655
e, %L7…7…7…7…
LT……………………
E, GPa71.0271.0271.0271.0271.0271.0271.0271.02
Ec, GPa72.3972.3972.3972.3972.3972.3972.3972.39
G, GPa26.8926.8926.8926.8926.8926.8926.8926.89
ν0.330.330.330.330.330.330.330.33
ρ, kg/m³27962796279627962796279627962796

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

°CF_tuF_tyF_cyF_suF_bruF_bry
-184117.8117.6
-129110110
-73105.5105.6
-18102.9102.8
3898.698.999.899.897.299.5
9389.291.294.79787.596.1
14974.27980.584.677.884.3
20445.75050.558.253.158.5
2619.919.820.227.724.323.1
31611.811.815.614.5

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.