PREN 6032 : 200P1
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF THE GLASS TRANSITION TEMPERATURES
Hardcopy , PDF
21-12-2023
English
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 Scope
2 Normative references
3 Definitions
4 Principle of the method
5 Designation of the method
6 Apparatus
7 Test specimen
8 Procedure
9 Presentation of the results
10 Test report
Annex A - Equipment
Gives a method to determine the apparent glass transition temperatures of non metallic materials. Applies to unidirectional tape and woven fabric reinforced plastic or plastic materials like neat resin or adhesive for comparison of the influence on the glass transition temperature resulting from processing-parameters of non metallic parts, for compatibility tests for checking co-curing effects of different prepreg types or with adhesive.
| Committee |
AIB/TF6
|
| DocumentType |
Draft
|
| Pages |
9
|
| ProductNote |
Superseded by EN 6032:2015
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 6032:2016-02 | Identical |
| PREN 2642 : 200P1 | AEROSPACE SERIES - STRUCTURAL ADHESIVE SYSTEMS - ADHESIVE FILM - TECHNICAL SPECIFICATION |
| PREN 2833-3 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP 180 DEGREES C FOR CONTINUOUS USE UP TO 120 DEGREES C |
| BS EN 2833-005:2013 | Aerospace series. Glass fibre thermosetting preimpregnates. Technical specification Glass fabric/phenolic resin preimpregnate |
| PREN 6044-2 : 200P1 | AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - QUALIFICATION PROGRAMM/BATCH RELEASE TESTING - UNIDIRECTIONAL TAPE 180 DEGREE C CURING CLASS |
| PREN 2833-5 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 5: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| PREN 2833-1 : 200P2 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS |
| PREN 6044-1 : 200P1 | AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS |
| I.S. EN 2833-005:2013 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| SAE AMS 2950/1 : 2008(R2019) | PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS |
| UNI EN 2833-005 : 2014 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| EN 2833-005:2013 | Aerospace series - Glass fibre thermosetting preimpregnates - Technical specification - Part 005: Glass fabric/phenolic resin preimpregnate |
| SAE AMS 2950/1 : 2008 | PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
| PREN 2565 : 200P2 | AEROSPACE SERIES - PREPARATION OF CARBON FIBRE REINFORCED RESIN PANELS FOR TEST PURPOSES |
| PREN 2823 : 200P2 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS |
| EN 2374:1991 | Aerospace series - Glass fibre reinforced mouldings and sandwich composites - Production of test panels |
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