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In Environmental Stress Screening
(ESS), When To Do Vibration
Environmental stress screening of a product is a process which involves the application of one
or more specific types of environmental stresses for the purpose of precipitating to hard failure,
latent, intermittent, or incipient defects or flaws which would cause product failure in the use
environment. The stress may be applied in combination or in sequence on an accelerated basis
but within product design capabilities.
Our requirements to improve the operational performance of End-Units while reducing their
operating and support costs can be met only by improving their quality and reliability. ESS has
been shown to be a significant aid towards meeting these objectives.
ESS is a cost-effective means of improving quality and reliability of electrical, electronic,
electro-optical, electromechanical assemblies and systems at a time when defect removal is
relatively inexpensive. Random Vibration and Temperature Cycling have proven to be the most
successful forms of ESS in terms of flaw precipitation.
ESS is a process rather than a test in the normal accept/reject sense. Those participating in the
effort, including the contractor, should never be led to believe that a “failure” is bad and would
be held against them. ESS is intended to stimulate defects, not to simulate the operating
environment, and therefore, factory “failures” are encouraged. The root causes of ESS failures
need to be found and corrected before there is a complete process.
Today, true random and quasi-random vibration are used almost exclusively for ESS. True
random vibration, which is well known in the ESS community, applies all frequencies in a
certain bandwidth (usually 20 to 2000 HZ) and is neither cyclic nor repetitive. Quasi-random
vibration, on the other hand, is a relatively new technology using pneumatically driven vibrators
which generate repetitive pulses. For screening applications, several (Usually 4 to 6) of these
vibrators are attached to a specially designed shaker table which is allowed to vibrate in multiple
axes simultaneously. This complex motion (6 degrees of freedom vibration–3 linear axes and 3
rotational axes) is very effective in finding all types of flaws.
It is not difficult to visualize that the complex interactions possible under random vibration can
induce a wider variety of relative motions in an assembly. As indicated by Table 1, vibration is
the area of stressing that normally precipitates latent assembly flaws caused by the undesired
relative motion of parts, wires, structural elements, etc., as well as mechanical flaws that lead to
propagating cracks.
As indicated in Table 1, some types of flaws may be precipitated to failures by either thermal
cycling or random vibration. However, it is important to note that thermal cycling and random
vibration are synergistic. For example, thermal cycling following random vibration sometimes
leads to detection of vibration induced failures that were not apparent immediately. There have
been reported cases where a very small flaw did not propagate to the point of detectability during
random vibration, but advanced to the point of detectability during subsequent thermal cycling.
Hilaire Ananda Perera
http://www.linkedin.com/in/hilaireperera
Ref: ESS Guidelines July 1993; A Tri-Service (Army, Navy, Air Force) Technical Brief

1
The combined efforts (synergism) between vibration and thermal cycling suggests that
concurrent application of the two stress types may be desirable. This combined environment is
in fact sometimes used in ESS, but more often is avoided because it requires more elaborate
facilities. Also, concurrent application of random vibration and thermal cycling can make it
difficult to determine what caused a defect so that corrective action can be taken.
If random vibration and thermal cycling are to be conducted sequentially, random vibration
would usually be done first. A more effective sequence would be five minutes of random
vibration prior to thermal cycling, and another five minutes of random vibration following.

Table 1: Screening Environments Versus Typical Failure Mechanics

SCREENING ENVIRONMENT
Thermal Cycling
•

Particle Contamination

•

Chaffed, Pinched Wires

•

Defective Crystals

Component
Incorrectly Installed

•

Mixed Assemblies

•

Wrong Component

•

•

Adjacent Boards
Rubbing

Hermetic Seal
Failure

•

Chemical
Contamination

•
•
•

TYPE OF FAILURES

Vibration

•

Component
Parameter Drift
PWA Open / Shorts

Thermal or Vibration
•

Defective Solder
Joints

•

Loose Hardware

•

Defective Components

•

Fasteners

•

Broken Component

Two Components
Shorting

•

Surface Mount
Technology Flaws

•

Loose Wire

•

Improperly Etched
PWAs

•

Defective Harness
Termination

•

Poorly Bonded
Component

•

Improper Crimp

•

•

Inadequately Secured
Parts

Poor Bonding

•

•

Mechanical Flaws

Hairline Cracks in
Parts

•

Improperly Seated
Connectors

•

Out-Of-Tolerance
Parts

Hilaire Ananda Perera
http://www.linkedin.com/in/hilaireperera
Ref: ESS Guidelines July 1993; A Tri-Service (Army, Navy, Air Force) Technical Brief

2

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Vibration before thermal cycling in ESS

  • 1. In Environmental Stress Screening (ESS), When To Do Vibration Environmental stress screening of a product is a process which involves the application of one or more specific types of environmental stresses for the purpose of precipitating to hard failure, latent, intermittent, or incipient defects or flaws which would cause product failure in the use environment. The stress may be applied in combination or in sequence on an accelerated basis but within product design capabilities. Our requirements to improve the operational performance of End-Units while reducing their operating and support costs can be met only by improving their quality and reliability. ESS has been shown to be a significant aid towards meeting these objectives. ESS is a cost-effective means of improving quality and reliability of electrical, electronic, electro-optical, electromechanical assemblies and systems at a time when defect removal is relatively inexpensive. Random Vibration and Temperature Cycling have proven to be the most successful forms of ESS in terms of flaw precipitation. ESS is a process rather than a test in the normal accept/reject sense. Those participating in the effort, including the contractor, should never be led to believe that a “failure” is bad and would be held against them. ESS is intended to stimulate defects, not to simulate the operating environment, and therefore, factory “failures” are encouraged. The root causes of ESS failures need to be found and corrected before there is a complete process. Today, true random and quasi-random vibration are used almost exclusively for ESS. True random vibration, which is well known in the ESS community, applies all frequencies in a certain bandwidth (usually 20 to 2000 HZ) and is neither cyclic nor repetitive. Quasi-random vibration, on the other hand, is a relatively new technology using pneumatically driven vibrators which generate repetitive pulses. For screening applications, several (Usually 4 to 6) of these vibrators are attached to a specially designed shaker table which is allowed to vibrate in multiple axes simultaneously. This complex motion (6 degrees of freedom vibration–3 linear axes and 3 rotational axes) is very effective in finding all types of flaws. It is not difficult to visualize that the complex interactions possible under random vibration can induce a wider variety of relative motions in an assembly. As indicated by Table 1, vibration is the area of stressing that normally precipitates latent assembly flaws caused by the undesired relative motion of parts, wires, structural elements, etc., as well as mechanical flaws that lead to propagating cracks. As indicated in Table 1, some types of flaws may be precipitated to failures by either thermal cycling or random vibration. However, it is important to note that thermal cycling and random vibration are synergistic. For example, thermal cycling following random vibration sometimes leads to detection of vibration induced failures that were not apparent immediately. There have been reported cases where a very small flaw did not propagate to the point of detectability during random vibration, but advanced to the point of detectability during subsequent thermal cycling. Hilaire Ananda Perera http://www.linkedin.com/in/hilaireperera Ref: ESS Guidelines July 1993; A Tri-Service (Army, Navy, Air Force) Technical Brief 1
  • 2. The combined efforts (synergism) between vibration and thermal cycling suggests that concurrent application of the two stress types may be desirable. This combined environment is in fact sometimes used in ESS, but more often is avoided because it requires more elaborate facilities. Also, concurrent application of random vibration and thermal cycling can make it difficult to determine what caused a defect so that corrective action can be taken. If random vibration and thermal cycling are to be conducted sequentially, random vibration would usually be done first. A more effective sequence would be five minutes of random vibration prior to thermal cycling, and another five minutes of random vibration following. Table 1: Screening Environments Versus Typical Failure Mechanics SCREENING ENVIRONMENT Thermal Cycling • Particle Contamination • Chaffed, Pinched Wires • Defective Crystals Component Incorrectly Installed • Mixed Assemblies • Wrong Component • • Adjacent Boards Rubbing Hermetic Seal Failure • Chemical Contamination • • • TYPE OF FAILURES Vibration • Component Parameter Drift PWA Open / Shorts Thermal or Vibration • Defective Solder Joints • Loose Hardware • Defective Components • Fasteners • Broken Component Two Components Shorting • Surface Mount Technology Flaws • Loose Wire • Improperly Etched PWAs • Defective Harness Termination • Poorly Bonded Component • Improper Crimp • • Inadequately Secured Parts Poor Bonding • • Mechanical Flaws Hairline Cracks in Parts • Improperly Seated Connectors • Out-Of-Tolerance Parts Hilaire Ananda Perera http://www.linkedin.com/in/hilaireperera Ref: ESS Guidelines July 1993; A Tri-Service (Army, Navy, Air Force) Technical Brief 2