PREN 6041 : 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Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
AEROSPACE SERIES - NON-METALLIC MATERIALS - TEST METHOD - ANALYSIS ON NON-METALLIC MATERIALS (UNCURED) BY DIFFERENTIAL SCANNING CALORIMETRY (DSC)
Hardcopy , PDF
21-12-2023
English
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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Superseded by DIN EN 6041:2018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Withdrawn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 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] |
| 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 AMS 3970/5 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 5: PURCHASING SPECIFICATION FOR COMPANION NON-STRUCTURAL GLASS FIBER FABRIC PREPREG |
| SAE AMS2950/1 | Paste Adhesive for Core Restoration Part 1 - General Requirements |
| UNI EN 4106 : 2014 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| SAE AMS 3970/4 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 4: PURCHASING SPECIFICATION FOR FILM ADHESIVE |
| 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 |
| SAE AMS 2950/1 : 2008 | PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS |
| 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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