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2024-T861 Clad flat sheet and plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2024 / T861 / Clad flat sheet and plate
SpecificationsAMS-QQ-A-250/5
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.3.0, Table 3.2.3.0(e) (pdf page 78 of the chapter file)
Dimension bands4
Density2768 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 band0.000–0.500 in (0–12.7 mm)0.020–0.062 in (0.508–1.575 mm)0.063–0.249 in (1.6–6.325 mm)0.250–0.499 in (6.35–12.67 mm)
SpecificationAMS-QQ-A-250/5AMS-QQ-A-250/5AMS-QQ-A-250/5AMS-QQ-A-250/5
BasisSSSS
Ftu, MPaL461.9448.2482.6468.8
LT461.9441.3475.7468.8
Fty, MPaL420.6406.8448.2427.5
LT420.6399.9441.3427.5
Fcy, MPaL420.6406.8448.2427.5
LT441.3420.6461.9448.2
Fsu, MPaL262248.2268.9268.9
LT262248.2268.9268.9
Fbru (e/D = 1.5), MPaL717.1682.6737.7723.9
LT717.1682.6737.7723.9
Fbru (e/D = 2.0), MPaL923.9882.5951.5937.7
LT923.9882.5951.5937.7
Fbry (e/D = 1.5), MPaL606.7579.2641.2620.5
LT606.7579.2641.2620.5
Fbry (e/D = 2.0), MPaL717.1682.6751.5723.9
LT717.1682.6751.5723.9
e, %L…………
LT4344
E, GPa72.3972.3972.3972.39
Ec, GPa75.1573.7773.7775.15
ν0.330.330.330.33
ρ, kg/m³2768276827682768

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
3897.997.597.498.598.499.6
9389.390.188.79092.597.2
14981.682.882.480.484.392.1
20471.169.772.568.371.979.1
2650.949.247.550.654.556.6
31628.825.321.624.829.932.9

Factors in percent of the room-temperature allowable.

Other 2024 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.