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Global 企业标准 D406A 固体火箭发动机壳体用钢 and Mechanical Properties, Chemical Element, Cross Reference.

Datasheet for: Metals: D406A / D406A
Category Grade Standard Region/Area Standard Content
Metals D406A -- Global 固体火箭发动机壳体用钢

Chemical composition(mass fraction)(wt.%) of the D406A

Element Min Max Similar
C 0.2700 0.3200 -
Mn 0.7000 1.0000 -
Si 1.4000 1.7000 -
S - 0.0100 -
P - 0.0130 -
Ni - 0.2500 -
Cr 1.0000 1.3000 -
Mo 0.4000 0.5500 -
V 0.0800 0.1500 -
Cu - 0.2500 -

Mechanical Properties of steel grade D406A

Yield
Rp0.2 (MPa)
Tensile
Rm (MPa)
Impact
KV/Ku (J)
Elongation
A (%)
Reduction in cross section on fracture
Z (%)
As-Heat-Treated Condition Brinell hardness (HBW)
441 (≥) 744 (≥) 34 44 34 Solution and Aging, Annealing, Ausaging, Q+T,etc 341

Physical Properties of steel grade D406A

Temperature
(°C)
Modulus of elasticity
(GPa)
Mean coefficient of thermal expansion 10-6/(°C) between 20(°C) and Thermal conductivity
(W/m·°C)
Specific thermal capacity
(J/kg·°C)
Specific electrical resistivity
(Ω mm²/m)
Density
(kg/dm³)
Poisson’s coefficient, ν
33 - -     0.22 -  
298 649 - 41.3 142   -  
981 - 23 42.2   433 422

Heat Treatment of steel grade D406A

Heat treated : 1251°C - 1257°C

Technological Curves of steel grade D406A

Cross Reference Table (Equivalent Grade) of D406A

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