PREN 3443 : 200P2
Withdrawn
Withdrawn
AEROSPACE SERIES - TITANIUM TI-P99003 - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM - 570 MPA <= R[M] <= 730 MPA
Available format(s)
Hardcopy , PDF
Language(s)
English
Withdrawn date
07-23-2013
US$53.45
Excluding Tax where applicable
0 Introduction
1 Scope and field of application
2 References
Covers the requirements relating to sheet and strip, hot rolled, a <= 6 mm, annealed, 570 MPa <= R[m] <= 730 MPa in titanium TI-P99003 for aerospace applications.
| Committee |
C5
|
| DevelopmentNote |
Supersedes PREN 2527. (10/2002)
|
| DocumentType |
Draft
|
| Pages |
5
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| Supersedes |
| Standards | Relationship |
| DIN EN 3443:1992-12 (Draft) | Identical |
| 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 |
| I.S. EN 4632-006:2013 | AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF 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 |
Summarise
US$53.45
Excluding Tax where applicable