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England B.S. S117 Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch) and Mechanical Properties, Chemical Element, Cross Reference.

Datasheet for: Metals: S117 / S 117
Category Grade Standard Region/Area Standard Content
Metals S 117 BS 2S 117 England Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)

Chemical composition(mass fraction)(wt.%) of the S 117

Element Min Max Similar

Mechanical Properties of steel grade S 117

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)
423 (≥) 549 (≥) 42 41 22 Solution and Aging, Annealing, Ausaging, Q+T,etc 434

Physical Properties of steel grade S 117

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
21 - -     0.14 -  
755 471 - 21.3 443   -  
229 - 14 43.2   313 233

Heat Treatment of steel grade S 117

Heat treated : 1627°C - 1164°C

Technological Curves of steel grade S 117

Cross Reference Table (Equivalent Grade) of S 117

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