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BS EN 3532:2025 | British Standards

Standards Shop | ICS 49 | ICS 49.025 |  ICS 49.025.10

49.025.10 Steels

Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa

Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa

BS EN 3532:2025

Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa


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ISBN: 9780539321272

Keywords:
Solution heat treatment, Precipitation hardening, Alloy steels, Dimensions, Defects, Elongation, Vacuum melting, Air transport engineering, Tensile strength, Impact strength, Proof stress, Grain size, Steels, Heat treatment, Sheet materials, Hardness, Chemical composition, PDF
Publication Date17 Sep 2025
Product SKU30494185
ISBN9780539321272
BSI CodeBS EN 3532:2025
No. of pages12
ReplacesBS EN 3532:2007
PublisherBritish Standards Institution
Identical National Standard to:
  • EN 3532




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