• There are no items in your cart
We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
Dismiss alert

PREN 6062 : 200P1

Current

Current

The latest, up-to-date edition.

AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - FLATWISE TENSILE TEST OF COMPOSITE SANDWICH PANEL

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-11-1995

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

Gives the flatwise tensile test, which is the procedure for the determination of the tensile strength, perpendicular to the honeycomb sandwich panels. The specimen is designed to fail in one of the core to skin bonds. Also can be used to obtain compatibility and strength data on unidirectional and woven fabric laminates, structural adhesives and epoxy resin used for repair purposes.

Committee
AIB/TF6
DocumentType
Draft
Pages
10
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Current

SAE AMS 2950/1 : 2008 PASTE ADHESIVE FOR CORE RESTORATION - 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 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS
SAE AMS 2950/1 : 2008(R2019) PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS

PREN 2743 : 200P1 AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING
PREN 2823 : 200P2 AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS
PREN 2419 : 200P3 AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T351 - PLATE - 6 MM < A <= 80 MM
PREN 2334 : 1995 CHROMIC-SULPHURIC ACID PICKLE OF ALUMINIUM AND ALUMINIUM ALLOYS

View more information
£88.41
Excluding VAT

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.