Tools › Materials › Aluminum › 7049/7149-T73 Die forging

7049/7149-T73 Die forging: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7049/7149 / T73 / Die forging
SpecificationsAMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.3.0, Table 3.7.3.0(c) (pdf page 307 of the chapter file)
Dimension bands5
Density2851 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)4.001–5.000 in (101.6–127 mm)
SpecificationAMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771
BasisABABABABAB
Ftu, MPaL489.5510.2482.6503.3475.7496.4468.8489.5461.9482.6
LT489.5…482.6…482.6…482.6…468.8…
ST…………………………
Fty, MPaL413.7441.3406.8434.4399.9420.6393413.7379.2406.8
LT420.6…413.7…413.7…413.7…399.9…
ST…………………………
Fcy, MPaL427.5455.1420.6448.2413.7434.4406.8427.5393420.6
LT…………………………
ST386.1413.7379.2406.8372.3393365.4386.1351.6379.2
Fsu, MPaL275.8282.7268.9282.7268.9275.8262275.8255.1268.9
LT275.8…268.9…268.9…262…255.1…
ST275.8282.7268.9282.7268.9275.8262275.8255.1268.9
Fbru (e/D = 1.5), MPaL689.5723.9682.6710.2675.7703.3661.9689.5655682.6
LT689.5…682.6…675.7…661.9…655…
ST689.5723.9682.6710.2675.7703.3661.9689.5655682.6
Fbru (e/D = 2.0), MPaL910.1951.5896.3937.7882.5923.9868.7910.1861.8896.3
LT910.1…896.3…882.5…868.7…861.8…
ST910.1951.5896.3937.7882.5923.9868.7910.1861.8896.3
Fbry (e/D = 1.5), MPaL565.4565.4517.1551.6510.2537.8503.3524482.6517.1
LT565.4…517.1…510.2…503.3…482.6…
ST565.4565.4517.1551.6510.2537.8503.3524482.6517.1
Fbry (e/D = 2.0), MPaL682.6682.6627.4668.8620.5648.1606.7641.2586.1627.4
LT682.6…627.4…620.5…606.7…586.1…
ST682.6682.6627.4668.8620.5648.1606.7641.2586.1627.4
e, %L7777777777
LT3…3…3…2…2…
ST…………………………
E, GPa70.3370.3370.3370.3370.3370.3370.3370.3370.3370.33
Ec, GPa73.7773.7773.7773.7773.7773.7773.7773.7773.7773.77
G, GPa26.8926.8926.8926.8926.8926.8926.8926.8926.8926.89
ν0.330.330.330.330.330.330.330.330.330.33
ρ, kg/m³2851285128512851285128512851285128512851

Effect of Temperature

The handbook maps no temperature-effect figure to this table.

Other 7049/7149 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.