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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.10 Steels>BS EN 3528:2013 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa
immediate downloadReleased: 2013-01-31
BS EN 3528:2013 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa

BS EN 3528:2013

Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa

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Standard number:BS EN 3528:2013
Pages:12
Released:2013-01-31
ISBN:978 0 580 77028 9
Status:Standard
DESCRIPTION

BS EN 3528:2013


This standard BS EN 3528:2013 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa is classified in these ICS categories:
  • 49.025.10 Steels
This standard specifies the requirements relating to: Steel X2NiCoMo18-8-5 (1.6359) Vacuum induction melted and vacuum arc remelted Solution treated and precipitation treated Bar a or D ? 150 mm 1 750 MPa ? Rm ? 2 000 MPa for aerospace applications. NOTE Other common designation: UNS: K92890, Marage 250, AECMA: FE-PA95, ASD-STAN: FE-PM2701, AIR: E-Z2NKD18, BS: S 162.
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