PREN 2850 : 200P2
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION
Hardcopy , PDF
11-12-2023
English
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 Scope
2 Normative references
3 Principle of the method
4 Definitions
5 Designation
6 Test pieces
7 Apparatus
8 Conditioning
9 Procedure
10 Calculation of results
11 Validity
12 Test report
Normative annex A
Normative annex B
Informative annex C
Defines a method for the determination of stress at failure and Young's modulus in compression of carbon thermosetting resin unidirectional laminates.
| Committee |
C7
|
| DocumentType |
Draft
|
| Pages |
14
|
| ProductNote |
Superseded by EN 2850:2017
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 2850:1998-04 (Draft) | Identical |
| PREN 6044-2 : 200P1 | AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - QUALIFICATION PROGRAMM/BATCH RELEASE TESTING - UNIDIRECTIONAL TAPE 180 DEGREE C CURING CLASS |
| 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] |
| PREN 6044-1 : 200P1 | AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS |
| I.S. EN ISO 14126:2000 | FIBRE-REINFORCED PLASTIC COMPOSITES - DETERMINATION OF COMPRESSIVE PROPERTIES IN THE IN-PLANE DIRECTION |
| SAE AMS 3970/1 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS |
| BS EN ISO 14126:1999 | Fibre-reinforced plastic composites. Determination of compressive properties in the in-plane direction |
| ISO 14126:1999 | Fibre-reinforced plastic composites — Determination of compressive properties in the in-plane direction |
| PREN 2489 : 1988 | FIBRE REINFORCED PLASTICS - DETERMINATION OF THE ACTION OF LIQUID CHEMICALS |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
| PREN 2859 : 1 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, CLOSE TOLERANCE NORMAL SHANK, SHORT THREAD, IN ALLOY STEEL, CADMIUM PLATED - CLASSIFICATION: 1 100 MPA (AT AMBIENT TEMPERATURE)/235 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 |
| PREN 3783 : 200P1 | AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES |
| EN 2744:1992 | Aerospace series - Non metallic materials - Preferred test temperatures |
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