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>UNE 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
sklademVydáno: 2025-10-01
UNE 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

UNE 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

Material aeroespacial. Acero X2NiCoMo18-8-5 (1.6359). Fundido en vacío y refundido por arco en vacío. Tratado en solución y precipitación. Placas a 6 mm < a <= 40 mm - 1 750 MPa <= Rm <= 2 000 MPa (Ratificada por la Asociación Española de Normalización en octubre de 2025.)

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Označení normy:UNE EN 3532:2025
Počet stran:11
Vydáno:2025-10-01
Status:Norma
DESCRIPTION

UNE EN 3532:2025

This document specifies the requirements relating to: Steel X2NiCoMo18-8-5 (1.6359) Vacuum induction melted and vacuum arc remelted Solution treated and precipitation treated Plates 6 mm < a d" 40 mm 1 750 MPa d" Rm d" 2 000 MPa for aerospace applications. NOTE ASD-STAN designation: FE-PM2701 Material number: 1.6359

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