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2024-T3, T3510, and T3511 Extruded bar, rod, and shapes: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2024 / T3, T3510, and T3511 / Extruded bar, rod, and shapes
SpecificationsAMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.3.0, Table 3.2.3.0(j) (pdf page 85 of the chapter file)
Dimension bands8
Density0.1 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 band0.000–0.249 in, area 0–20 in20.250–0.499 in, area 0–20 in20.500–0.749 in, area 0–20 in20.750–1.499 in, area 0–20 in21.500–2.999 in, area 0–25 in21.500–2.999 in, area 25– in23.000–4.499 in, area 0–25 in23.000–4.499 in, area 0–32 in2
SpecificationAMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3
BasisABABABABABSABS
Ftu, ksiL5761606260626570707468707468
LT5458565754565660555853545752
Fty, ksiL4247444744474654525448525448
LT3741384037393743394136394136
Fcy, ksiL3438373938404148495045495145
LT4145414440434047424439414338
Fsu, ksiL2931313230313335343633333532
LT2931313230313335343633333532
Fbru (e/D = 1.5), ksiL8490788178808490889386869184
LT8490788178808490889386869184
Fbru (e/D = 2.0), ksiL1081149810197101105113111118108109115106
LT1081149810197101105113111118108109115106
Fbry (e/D = 1.5), ksiL6168555955595767636659626557
LT6168555955595767636659626557
Fbry (e/D = 2.0), ksiL7179677167716981778071757869
LT7179677167716981778071757869
e, %L121212…12…10…10…810…8
LT……………………………………
E, Msi10.810.810.810.810.810.810.810.810.810.810.810.810.810.8
Ec, Msi1111111111111111111111111111
G, Msi4.14.14.14.14.14.14.14.14.14.14.14.14.14.1
ν0.330.330.330.330.330.330.330.330.330.330.330.330.330.33
ρ, lb/in30.10.10.10.10.10.10.10.10.10.10.10.10.10.1

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_ty
-300111.6118.5
-200105.3108.3
-100103103.6
0101.6102
10098.998.9
20092.493.9
30083.987.4
40074.577.7
50043.851.6
60022.526.9
7001214
8008

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.