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7475-T7351 Plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7475 / T7351 / Plate
SpecificationsAMS 4202
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.10.0, Table 3.7.10.0(c) (pdf page 461 of the chapter file)
Dimension bands6
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 band0.250–1.500 in (6.35–38.1 mm)1.501–2.000 in (38.13–50.8 mm)2.001–2.500 in (50.83–63.5 mm)2.501–3.000 in (63.53–76.2 mm)3.001–3.500 in (76.23–88.9 mm)3.501–4.000 in (88.93–101.6 mm)
SpecificationAMS 4202AMS 4202AMS 4202AMS 4202AMS 4202AMS 4202
BasisABABABABABAB
Ftu, MPaL482.6496.4482.6489.5468.8482.6468.8475.7441.3461.9441.3455.1
LT489.5503.3482.6496.4468.8482.6468.8475.7441.3468.8441.3461.9
ST455.1482.6448.2475.7448.2475.7448.2468.8434.4461.9434.4455.1
Fty, MPaL406.8427.5399.9413.7386.1406.8386.1399.9358.5386.1358.5372.3
LT413.7427.5399.9420.6386.1406.8386.1399.9358.5386.1358.5372.3
ST372.3393365.4386.1365.4386.1365.4379.2344.7365.4344.7358.5
Fcy, MPaL399.9413.7386.1406.8372.3393365.4379.2337.8365.4337.8351.6
LT420.6434.4413.7434.4399.9420.6399.9413.7372.3399.9372.3386.1
ST427.5441.3413.7434.4399.9420.6399.9413.7372.3399.9372.3386.1
Fsu, MPaL282.7289.6289.6296.5282.7289.6282.7289.6268.9289.6268.9282.7
LT282.7289.6289.6296.5282.7289.6282.7289.6268.9289.6268.9282.7
ST282.7289.6289.6296.5282.7289.6282.7289.6268.9289.6268.9282.7
Fbru (e/D = 1.5), MPaL703.3723.9710.2730.8696.4717.1696.4710.2668.8703.3668.8696.4
LT703.3723.9710.2730.8696.4717.1696.4710.2668.8703.3668.8696.4
ST703.3723.9710.2730.8696.4717.1696.4710.2668.8703.3668.8696.4
Fbru (e/D = 2.0), MPaL910.1937.7923.9951.5903.2930.8903.2923.9861.8917861.8903.2
LT910.1937.7923.9951.5903.2930.8903.2923.9861.8917861.8903.2
ST910.1937.7923.9951.5903.2930.8903.2923.9861.8917861.8903.2
Fbry (e/D = 1.5), MPaL558.5579.2565.4592.9558.5579.2558.5579.2530.9565.4530.9551.6
LT558.5579.2565.4592.9558.5579.2558.5579.2530.9565.4530.9551.6
ST558.5579.2565.4592.9558.5579.2558.5579.2530.9565.4530.9551.6
Fbry (e/D = 2.0), MPaL668.8696.4668.8703.3655689.5655682.6613.6661.9613.6641.2
LT668.8696.4668.8703.3655689.5655682.6613.6661.9613.6641.2
ST668.8696.4668.8703.3655689.5655682.6613.6661.9613.6641.2
e, %L1010101010101010101099
LT998888888877
ST444444333333
E, GPa71.0271.0271.0271.0271.0271.0271.0271.0271.0271.0271.0271.02
Ec, GPa73.0873.0873.0873.0873.0873.0873.0873.0873.0873.0873.0873.08
G, GPa26.8926.8926.8926.8926.8926.8926.8926.8926.8926.8926.8926.89
ν0.330.330.330.330.330.330.330.330.330.330.330.33
ρ, kg/m³279627962796279627962796279627962796279627962796

Effect of Temperature

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

Other 7475 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.