PREN 6043 : 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Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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 - THERMOSETTING RESIN SYSTEMS - TEST METHOD - DETERMINATION OF GEL TIME AND VISCOSITY
Hardcopy , PDF
23-07-2013
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 - Equipments
Gives the procedure for the determination of the viscosity and gel time of thermosetting resin systems by using several experimental techniques. The results obtained under dynamic and/or isothermal conditions, may be used to control the processing of resin systems during the cure cycle.
| Committee |
AIB/TF6
|
| DocumentType |
Draft
|
| Pages |
16
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| Standards | Relationship |
| DIN EN 6043:1996-04 (Draft) | Identical |
| PREN 6085 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - EPOXY SURFACING FILMS |
| PREN 6084 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - SURFACING FILMS - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS |
| SAE AMS 3970/3 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES 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 |
| 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 AMS 3970/1 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES 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] |
| 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 |
| SAE AMS 2950/1 : 2008 | PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS |
| SAE AMS 2950/1 : 2008(R2019) | PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS |
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