PREN 6041 : 200P1
Withdrawn
AEROSPACE SERIES - NON-METALLIC MATERIALS - TEST METHOD - ANALYSIS ON NON-METALLIC MATERIALS (UNCURED) BY DIFFERENTIAL SCANNING CALORIMETRY (DSC)
Hardcopy , PDF
English
12-21-2023
1 Scope
2 Normative references
3 Definitions
4 Principle of the method
5 Designation of the method
6 Apparatus
7 Test specimens
8 Procedure
9 Presentation of the results
10 Test report
Annex A - Equipment
Gives the procedure for determining the curing-characteristic and glass transition temperature of non-metallic materials (e.g. preimpregnated and neat resin systems, adhesives) for aerospace use by Differential Scanning Calorimetry (DSC). The results that are obtained by this method may be useful for: - assessment of the ageing behavior of the resin; - assessment of the condition of the resin; - derivation of the optimum cure (only together with other test methods e.g. T[g] determination).
| Committee |
AIB/TF6
|
| DocumentType |
Draft
|
| Pages |
11
|
| ProductNote |
Superseded by DIN EN 6041:2018
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| BS EN 4106:2013 | Aerospace series. Non-metallic materials. Structural adhesive systems. Paste adhesive. Technical specification |
| PD CEN/TR 14548:2003 | Adhesives. Guide to test methods and other standards for the general requirements, characterization and safety of structural adhesives |
| SAE AMS3970/3A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Carbon Prepreg |
| 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 |
| PREN 4106 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| SAE AMS2950/1 | Paste Adhesive for Core Restoration Part 1 - General Requirements |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| I.S. CEN TR 14548:2003 | ADHESIVES - GUIDE TO TEST METHODS AND OTHER STANDARDS FOR THE GENERAL REQUIREMENTS, CHARACTERIZATION AND SAFETY OF STRUCTURAL ADHESIVES |
| EN 4106:2013 | Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification |
| I.S. EN 4106:2013 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| CEN/TR 14548:2003 | Adhesives - Guide to test methods and other standards for the general requirements, characterization and safety of structural adhesives |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
| PREN 2559 : 1988 | CARBON FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF THE RESIN AND FIBRE CONTENT AND THE MASS OF FIBRE PER UNIT AREA |
| EN 2331:1993 | Aerospace series - Textile glass fibre preimpregnates - Test methods for the determination of the resin and fibre content and mass of fibre per unit area |
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