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PREN 3442 : 200P2

Current
Current

The latest, up-to-date edition.

AEROSPACE SERIES - TITANIUM TI-P99002 - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM - 390 MPA <= R[M] <= 540 MPA
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-26-1993

Publisher

Aerospace & Defence Industries Association of Europe

0 Introduction
1 Scope and field of application
2 References

Covers the requirements relating to sheet and strip, hot rolled, a <= 6 mm, annealed, 390 MPa <= R[m] <= 540 MPa in titanium TI-P99002 for aerospace applications.

Committee
C5
DevelopmentNote
Supersedes PREN 2526. (10/2002)
DocumentType
Draft
Pages
5
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Current
Supersedes

Standards Relationship
DIN EN 3442:1992-12 (Draft) Identical

UNI EN 4632-006 : 2014 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS
I.S. EN 4632-006:2013 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS
09/30199811 DC : 0 BS EN 4632-006 - AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 6: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
BS EN 4632-006:2013 Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys
EN 4632-006:2013 Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys
PREN 4632-006 : DRAFT 2008 WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS

EN 2338 : 2001 Aerospace series - Sheets, hot rolled in titanium and titanium alloys - Thickness 0,8 mm < = a < = 6 mm - Dimensions

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Hardcopy - English
PDF - English
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