Aerospace & defence

Materials Testing Systems for Aerospace and Defence

From metallic coupons and composite laminates to bonded joints and fasteners, DAK testing systems support mechanical characterisation for aerospace laboratories. Bring the specimen, loading method, measurement and reporting requirements together in a complete test configuration.

DAK testing systems

Connect material characterisation with the right platform

DAK Series 7200 universal testing machine

Flagship platform

Series 7200

Our flagship universal testing platform brings together specimen handling, force and strain measurement, flexible test programming and analysis. Configure the frame and accessories around the materials, components and test methods in your laboratory.

DAK Series 9000 universal testing machine

Series 9000

A universal testing platform for routine laboratory and production checks, with standalone Console or PC operation. Select the frame, grips and measurement arrangement for your defined test workflow.

Fatigue and repeated-load programmes

When the requirement concerns repeated loading, define the waveform, control mode, force range, frequency and specimen arrangement. DAK fatigue systems provide a separate platform for cyclic testing of coupons and components.

Materials and components

Choose the specimen and the property you need

Metallic materials and coupons

For alloy sheet, bar and machined specimens, define the material condition, test direction and required tensile or compression properties. Include the measurement length and any specified test temperature.

Composite laminates

Fibre direction, lay-up and specimen preparation influence the test configuration. Tensile, compression, flexural and shear methods use distinct loading arrangements to characterise the laminate.

Sandwich cores and panels

Core compression, flatwise tension and sandwich flexure examine different aspects of the construction. Specify whether the test concerns the core, a facing, their bond or the assembled sandwich.

Bonded joints and interfaces

Joint geometry and adherend stiffness influence the way load enters a bond. Define the required peel or shear arrangement and the interface being evaluated.

Fasteners, cables and terminals

A fastener specimen, cable and terminated assembly each need their own load-transfer arrangement. Include the dimensions, end details and required tensile, proof-load or other mechanical test.

Technical textiles and flexible materials

For flexible specimens used in aerospace applications, define the construction, test direction, gripping length and expected extension. The material or seam test determines the holding arrangement.

Your testing programme

Keep the test result connected to the engineering question

Composite tensile properties

Specimen orientation and preparation, secure gripping, alignment and the specified strain-measurement approach.

Composite compression

The method-specific loading fixture, specimen geometry and strain measurement used for the required compression result.

Metallic tensile properties

Material condition, specimen dimensions, required strength/elongation results and the applicable measurement arrangement.

Repeated loading

A fatigue test specification covering loading mode, waveform, force range, frequency and the reported result.

For a component or assembly test, include the drawing and the intended load path. A material coupon and a complete assembly answer different engineering questions, even when they use the same base material.

Configuration

Specify the complete test arrangement

Specimen holding and load path

Identify gripping surfaces, tabs, fixture contacts or end fittings. The arrangement must introduce the intended load while leaving the required specimen region available for measurement.

Force, strain and working space

Define the force range, specimen dimensions and required travel. Select the load cell and specimen-strain measurement around the properties and accuracy requirements of the method.

Environment and documentation

Include test temperature and conditioning, specimen identification, required outputs and your laboratory's calibration/documentation requirements. These belong in the configuration discussion alongside the hardware.

Laboratory workflow

Plan beyond a single test

Comparing materials or production batches

Use a defined specimen, orientation and test method so results can be compared on the same basis. Include the identification and report fields your team uses to connect each result with its material or batch.

Expanding the laboratory's test range

List the immediate test programme and the additional materials or loading methods you expect to introduce. This helps define the frame, fixtures, measurement options and software workflow as one system.

Methods and standards

Find the method for your aerospace material

Explore the full set of aerospace and defence method references below. Use your required designation, edition and programme-specific requirements when preparing the testing specification.

Also testedParachute & aircrew textiles

ASTM A931 / control cable specs

Tensile

Breaking strength of aircraft control cables, wire rope and swaged terminals.

ASTM C297 / C393 / C365

Flexure & bend

Honeycomb sandwich panels — flatwise tension, beam flexure and core compression.

Showing 1–8 of 65 standards

Discuss your application

Build your aerospace testing requirement with DAK

Share the specimen, test method and required result so we can focus the discussion on the machine, fixtures and measurement your programme needs.

  • Material, specimen geometry, orientation and condition.
  • Required standard, edition or programme-specific test specification.
  • Loading mode, force range, displacement/strain needs and test conditions.
  • Required reporting, documentation, throughput and planned future tests.

For laboratories in India and international markets, include the installation location and your training, calibration and service requirements.