PREN 6064 : 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Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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 - ANALYSIS OF NON-METALLIC MATERIALS (CURED) FOR THE DETERMINATION OF THE EXTENT OF CURE 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 Specimen
8 Procedure
9 Presentation of the results
10 Test report
Annex A - Equipment
Covers the procedure for the estimation of the extent of cure of certain non-metallic materials (e.g. adhesives, preimpregnated and neat resin systems) for aerospace use. The extent of cure is estimated by Differential Scanning Calorimetry (DSC) measurements of uncured (reference) and cured materials. Extra evidence on the extent of cure may be gained by combining results from this method with those obtained by other techniques.
| Committee |
AIB/TF6
|
| DocumentType |
Draft
|
| Pages |
10
|
| ProductNote |
Superseded by DIN EN 6064(2018-03)
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| Standards | Relationship |
| NF EN 6064 : 2017 PR | Identical |
| SAE AMS 2950/1 : 2008 | PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS |
| BS EN 4106:2013 | Aerospace series. Non-metallic materials. Structural adhesive systems. Paste adhesive. Technical specification |
| PREN 4106 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| 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 |
| EN 4106:2013 | Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification |
| 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] |
| I.S. EN 4106:2013 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| SAE AMS2950/1 | Paste Adhesive for Core Restoration Part 1 - General Requirements |
| 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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