PREN 3442 : 200P2
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
Hardcopy , PDF
English
26-05-1993
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 |
| 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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