UK B.S. BS S 127, S.127 Specialsteel Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in) and Mechanical Properties, Chemical Element, Cross Reference, Datasheet.
| Category | Class | Grade | Standard | Country | Application | 
|---|---|---|---|---|---|
| Steel Grades | Specialsteel | S.127 | B.S. | UK | Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in) | 
| C | Si | Mn | P | S | Cr | Ni | Mo | Ti | 
|---|---|---|---|---|---|---|---|---|
| ≤0.15 | 0.20 -1.00 | 0.50 -2.00 | ≤0.035 | ≤0.025 | 23.00 -26.00 | 16.00 -19.00 | ≤ ≥ | ≤4×C | 
| 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) | 
|---|---|---|---|---|---|---|
| 459 (≥) | 245 (≥) | 43 | 13 | 33 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 431 | 
| 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 | 
|---|---|---|---|---|---|---|---|
| 44 | - | - | 0.12 | - | |||
| 629 | 145 | - | 12.3 | 431 | - | ||
| 846 | - | 11 | 21.2 | 433 | 244 | 
Heat treated : 1525°C - 1959°C
| BS S 127 | Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in) | BS-S-127.pdf | 
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