Testing standard

ASTM D7136 Drop-Weight Impact Damage Testing of Composites

Standard Test Method for Measuring the Damage Resistance of a Fiber-Reinforced Polymer Matrix Composite to a Drop-Weight Impact Event

Written and technically reviewed by Dak System Inc. engineeringLast reviewed

ASTM D7136 creates a controlled, repeatable impact damage in a composite plate by dropping a guided hemispherical mass onto it. It is not a strength test — its output is a damaged plate and a record of the strike. What that damage costs the laminate is measured afterwards by ASTM D7137.

At a glance

Test type
Compressionthe specimen is squeezed
Published by
ASTM
Edition
D7136/D7136M-25

From the test method to your testing system

Explore DAK equipment for ASTM D7136, then review the specimen and setup requirements below.

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01Understand the method

What the test does

A rectangular composite plate is clamped at its four corners over a support with a rectangular cut-out beneath it, leaving the centre free to flex. A guided mass carrying a 16 mm hemispherical impactor is released from a height calculated to deliver a specified energy. An instrumented tup records force and displacement through the strike, and a catch arrests the impactor on rebound so the plate is struck exactly once. The dent depth is then measured and the internal damage mapped by ultrasonic scanning.

What it measures, and why it matters

Strictly, its product is a damaged specimen rather than a number, and that is the point. Impact damage in a composite is mostly internal: a strike that leaves a dent an inspector would struggle to find can create a delamination many times larger inside the laminate, removing a substantial share of its compressive strength. That gap between what is visible and what has been lost — barely visible impact damage — is the central safety problem in composite structure. A metal panel struck by a dropped spanner dents visibly and keeps most of its strength; a composite panel struck the same way may look almost untouched and have lost a third of its compressive capability. Inspection intervals, allowable damage limits and repair thresholds all rest on that gap. This method makes that damage repeatably so that ASTM D7137 can measure what it cost, and the pair together is how damage tolerance is actually established.

02Prepare the specimen and test settings

Specimen and drop tower

This method's product is a damaged specimen. Everything is arranged so that the same damage can be made again tomorrow.

Plate
A rectangular laminate, clamped at four cornersClamped rather than gripped — the corners hold it down while the centre is free to respond.
Support
A rectangular cut-out beneath the plateIt defines the unsupported span and therefore how the plate flexes under the strike.
Impactor
Hemispherical, 16 mm diameterBlunt on purpose. A sharp tup would cut; this one delaminates, which is the damage aircraft structures actually get.
Energy
Scaled to thickness — commonly 6.7 J per mmScaling by thickness is what lets laminates of different thickness be compared at all.
Rebound catch
RequiredAn uncaught impactor strikes a second time and the specimen no longer represents one event.
Inspect ultrasonically before the next test
Map the damage areaDakBarely visible impact damage is mostly internal. What the eye sees understates what the laminate has lost.

The impactor MUST be caught after rebound. A second strike on an already-damaged plate produces a specimen that represents nothing, and it is easy to miss because the plate looks much the same.

Test speed

Energy, not speed
6.7 J per mm of specimen thickness — 33.5 J on the 5.0 mm laminate the method targetsNo rate of traverse is set anywhere in the method. Energy is the controlled quantity, and drop height follows from it.
Drop height and impact velocity
H = E / mg — 0.62 m for 33.5 J on the 5.5 kg impactor, arriving at about 3.5 m/sThe 5.5 ± 0.25 kg mass and the 16 ± 0.1 mm hemispherical tip are fixed by the method; the height and velocity are arithmetic from them.
Minimum drop
300 mm; below the energy that gives, use a 2.0 ± 0.25 kg impactor
Instrumented tup
Records force and displacement through the strikeThe force-time trace shows when delamination started, which the final damage cannot.
One strike per specimen
Always
Record the dent depth
After the plate has relaxedDakA composite recovers some indentation over minutes, so a depth read immediately overstates it.

03Build the test setup on a DAK machine

What the machine must be capable of

This part of the pair needs a drop tower rather than a universal frame: a guided mass, an adjustable height, an instrumented tup, and — mandatory rather than optional — a catch that arrests the impactor on rebound. The universal testing machine's role comes afterwards, in the compression-after-impact test the damaged plate is passed to. Ultrasonic inspection equipment is required too, because the damage that matters cannot be measured any other way.

The method sets no rate of traverse and could not, since the strike is over in milliseconds. It fixes energy instead, and the height follows. The impactor is 5.5 ± 0.25 kg carrying a 16 ± 0.1 mm hemispherical tip, and the potential energy is 6.7 J per millimetre of specimen thickness. On the 5.0 mm laminate the method targets that is 33.5 J, so the drop height H = E / mg is 0.62 m and the tup arrives at √(2gH), about 3.5 m/s. There is a floor as well: the fall must be at least 300 mm, and where the wanted energy cannot be reached from that height with the standard mass, a 2.0 ± 0.25 kg impactor is used instead. Mass, height and energy are the three numbers a report has to carry. Crosshead speed is not one of them.

Running ASTM D7136 on the Series 7200 and Series 9000

Dak verifies against whichever standard the method names, and where a class applies our frames sit a class tighter than it asks.

The method asks forDak supplies
CapacityNot a force test — the controlled quantity is impact ENERGY, commonly 6.7 J per mm of thicknessLoad cells from 1 kg to 60 ton on the Series 7200, and 0.5 to 100 kN on the Series 9000
Force accuracyASTM E4Verified to ASTM E4, and to ISO 7500-1 Class 0.5
GrippingA drop tower with a hemispherical 16 mm impactor, over a rectangular cut-out support with the plate clamped at four cornersWedge, vice-action, pneumatic and hydraulic grips, built to the specimen
Environment23 ± 2 °C standard laboratory atmosphere3009 series chambers, −150 °C to +400 °C — temperature only

04Run the test

How the test runs

  1. Cut rectangular plates from a balanced, symmetric laminate.
  2. Measure thickness and compute the required energy.
  3. Set drop mass and height to deliver it.
  4. Clamp the plate at four corners over the cut-out support.
  5. Confirm the rebound catch is armed.
  6. Release the impactor and record the force-time trace.
  7. Confirm only one strike occurred.
  8. Let the plate relax, then measure the dent depth.
  9. Ultrasonically scan the plate and record the damage area.
  10. Photograph both faces.
  11. Pass the plate to ASTM D7137 for the residual strength measurement.

05Calculate, report and interpret

Calculations

Impact energyE

E = m × g × h

m
drop mass, kg
g
9.81 m/s²
h
drop height, m

Set by choosing mass and height together. The same energy from a heavier mass at lower height is not identical in effect, which is why both are reported.

Normalised energy

Energy per unit thickness, commonly 6.7 J/mm

Scaling by thickness is what makes laminates of different thickness comparable.

Damage area

Measured by ultrasonic C-scan of the impacted plate

The visible dent is a small fraction of it. This is why the damage is called barely visible.

What the report has to contain

  • Reference to ASTM D7136 and the edition
  • Material, lay-up and cure schedule
  • Plate dimensions and measured thickness
  • Support cut-out dimensions and clamping arrangement
  • Impactor diameter and mass
  • Drop height and impact energy, and the energy per unit thickness
  • Force-time trace and peak force
  • Dent depth after relaxation
  • Damage area from ultrasonic inspection
  • Confirmation that only one strike occurred
  • Photographs of both faces

What goes wrong in practice

A second, uncaught strike is the classic invalidation and the easiest to miss, because a plate hit twice looks much like a plate hit once. The damage from two impacts is not the damage from one at twice the energy, so the specimen then represents nothing. Reading dent depth inconsistently is another, since it is one of the few things an inspector can see in service. Assessing the damage visually rather than ultrasonically understates it profoundly — that understatement is precisely the hazard the method exists to characterise.

06Compare methods and find answers

ASTM D7136 or ISO 6603-2

ASTM D7136ISO 6603-2
PurposeCreate controlled damage for a later testCharacterise puncture behaviour
Impactor16 mm hemisphericalHemispherical striker
Primary outputA damaged plate, plus the strike recordForce-deflection and puncture energy
Usually followed byASTM D7137 compression after impactNothing — it is the whole test

D7136 exists to make a specimen for D7137. ISO 6603 is a complete test in itself. Treating a D7136 result as a strength figure misunderstands what the method is for.

Questions we are asked about this test

What is ASTM D7136?

It is the ASTM method for creating a controlled drop-weight impact damage in a composite plate. A guided 16 mm hemispherical impactor is dropped onto a clamped plate at an energy scaled to its thickness. The output is a damaged specimen and a record of the strike, not a strength figure.

Why is it not a strength test?

Because the number that matters comes afterwards. Impact damage in a composite is mostly internal delamination that costs the laminate a great deal of compressive strength while leaving the surface almost unmarked. D7136 makes that damage repeatably; ASTM D7137 then compresses the plate to find out what it cost. Quoting a D7136 energy as though it were a material property misses the point of running it.

Why a blunt hemispherical impactor?

Because it delaminates rather than cuts, and delamination is the damage real structures actually receive. A dropped tool, a hailstone or a knock during maintenance spreads its energy over a blunt contact; the laminate absorbs it by separating between plies rather than by being penetrated. A sharp tup would produce a hole, which is a different and less dangerous kind of damage because you can see it.

What is barely visible impact damage?

It is the reason this pair of tests exists. A strike can leave a dent a millimetre deep that an inspector would struggle to find, while creating a delamination many times larger inside the laminate that removes a substantial share of its compressive strength. The eye sees almost nothing; an ultrasonic scan sees the real extent. That gap is the whole safety problem in composite structures.

Why must the impactor be caught after rebound?

Because a second strike on an already-damaged plate produces a specimen that represents no defined event at all. The damage from two impacts is not the damage from one at twice the energy, and it is easy to miss because the plate looks much the same either way. The rebound catch is mandatory equipment, not a refinement.

Why scale the energy to thickness?

Because a thicker laminate absorbs more energy before it delaminates, so a fixed joule figure would damage a thin plate severely and a thick one hardly at all. Normalising to energy per millimetre of thickness — commonly 6.7 J/mm — is what allows laminates of different thickness to be compared on equal terms.

Why measure the dent after the plate relaxes?

Because a composite recovers part of its indentation over the following minutes as the matrix relaxes. A depth read immediately after the strike overstates the permanent dent, sometimes considerably. Since dent depth is one of the few things an inspector can actually see in service, measuring it consistently matters.

The test it standardises

Industries that test to it

Other standards explained

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