EN 6032:2015
Current
The latest, up-to-date edition.
Aerospace series - Fibre reinforced plastics - Test method - Determination of the glass transition temperatures
25-11-2015
European foreword
1 Scope
2 Normative references
3 Terms and 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 (informative) - Equipment
This standard specifies a method to determine the apparent glass transition temperatures of non-metallic materials.This standard is applicable to unidirectional tape and woven fabric reinforced plastic or plastic materials like adhesive or neat resin 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.This standard does not give any directions necessary to meet health and safety requirements. It is the responsibility of the user of this standard to consult and establish appropriate health and safety precautions.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 6032. (12/2015)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| I.S. EN 6032:2015 | Identical |
| DIN EN 6032:2016-02 | Identical |
| BS EN 6032:2015 | Identical |
| NS EN 6032 : 2015 | Identical |
| NF EN 6032 : 2016 | Identical |
| UNI EN 6032 : 2016 | Identical |
| NEN EN 6032 : 2015 | Identical |
| PN EN 6032 : 2016 | Identical |
| SN EN 6032:2016 | Identical |
| NBN EN 6032 : 2015 | Identical |
| UNE-EN 6032:2015 | Identical |
| 93/706616 DC : 0 | PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| 99/701511 DC : DRAFT JAN 1999 | PREN 4106 - AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| 95/714421 DC : 0 | PREN 2833-3 - AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 180 DEGREE C FOR CONTINUOUS USE UP TO 120 DEGREE C |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| SAE AMS 3970/6 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2] |
| 95/714422 DC : 0 | PREN 2833-4 - AEROSPACE SERIES - GLASS FIBER THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREE C FOR CONTINUOUS USE UP TO 80 DEGREE C |
| PREN 2833-4 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| 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 2743:2001 | Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials |
| EN 2374:1991 | Aerospace series - Glass fibre reinforced mouldings and sandwich composites - Production of test panels |
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