elimination of s n in spacecraft assemblies presentation to the emaps workshop 17 th february 2010

27
Elimination of S Elimination of S n n in Spacecraft in Spacecraft Assemblies Assemblies Presentation to the EMAPS Presentation to the EMAPS Workshop Workshop 17 17 th th February 2010 February 2010

Upload: celine-plass

Post on 01-Apr-2015

217 views

Category:

Documents


0 download

TRANSCRIPT

Page 1: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Elimination of SElimination of Snn in in Spacecraft AssembliesSpacecraft Assemblies

Presentation to the EMAPS Presentation to the EMAPS Workshop Workshop

1717thth February 2010 February 2010

Page 2: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

About UsAbout Us

Site, Buildings and Facility Owned by Spur Site, Buildings and Facility Owned by Spur Group Group

Spur Group Owned by the Snowdon FamilySpur Group Owned by the Snowdon Family

Spur GroupSpur Group

Spur Electron Ltd (SEL)Spur Electron Ltd (SEL)

est. 1982est. 1982

Spur Information Solutions Ltd (SIS)Spur Information Solutions Ltd (SIS)

Page 3: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Spur Electron OverviewSpur Electron Overview

>

Spur Electron specialises in:-Spur Electron specialises in:-

All aspects of High Reliability component All aspects of High Reliability component engineering and procurement engineering and procurement

Component Assessment and Failure Component Assessment and Failure Analysis…Analysis…

Manufacture of hardware to ESA, NASA and Manufacture of hardware to ESA, NASA and Military StandardsMilitary Standards

Page 4: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Spur Electron OverviewSpur Electron Overview

Page 5: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Spur Electron OverviewSpur Electron Overview

Spur Electron specialises in:-Spur Electron specialises in:-

All aspects of High Reliability component All aspects of High Reliability component engineering and procurement engineering and procurement

Component Assessment and Failure Component Assessment and Failure Analysis…Analysis…

Manufacture of hardware to ESA, NASA and Manufacture of hardware to ESA, NASA and Military StandardsMilitary Standards

>

Page 6: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010
Page 7: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Spur Electron OverviewSpur Electron Overview

>

Spur Electron specialises in:-Spur Electron specialises in:-

All aspects of High Reliability component All aspects of High Reliability component engineering and procurement engineering and procurement

Component Assessment and Failure Component Assessment and Failure Analysis…Analysis…

Manufacture of hardware to ESA, NASA and Manufacture of hardware to ESA, NASA and Military StandardsMilitary Standards

Page 8: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010
Page 9: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

The Spur input to EMAPSThe Spur input to EMAPS

The title proposed for this input was:The title proposed for this input was:

““The elimination of SThe elimination of Snn in Spacecraft Assemblies.” in Spacecraft Assemblies.”

I would suggest a subtle change of title to :I would suggest a subtle change of title to :

““The minimisation of SThe minimisation of Snn in Spacecraft Assemblies” in Spacecraft Assemblies”

The complete The complete eliminationelimination of pure S of pure Snn in Spacecraft Hardware, even in Spacecraft Hardware, even today, is virtually impossible and will become even more difficult today, is virtually impossible and will become even more difficult in the future.in the future.

Page 10: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

What does ESA say What does ESA say about pure about pure SSnn ??

ESCC – 60 - 6.2.2.2 ESCC – 60 - 6.2.2.2 d1, “Pure Sd1, “Pure Snn used as a finish on leads, used as a finish on leads,

terminations and external surfaces of terminations and external surfaces of components and packages shall not be components and packages shall not be used”used”

e, “The use of pure Se, “The use of pure Snn in internal cavities in internal cavities may be authorised, on a case by case basis, may be authorised, on a case by case basis, based on a demonstration there is no based on a demonstration there is no alternative product alternative product and there is no and there is no risk!!risk!!””

Page 11: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Minimisation of pure SMinimisation of pure Snn in in Spacecraft HardwareSpacecraft Hardware

We have already heard that we face We have already heard that we face two major problems using pure Stwo major problems using pure Snn..

Tin Whiskers & Tin PestTin Whiskers & Tin Pest

Photo courtesy of Goddard Space Flight Center

Page 12: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Tin Whiskers & Tin Pest Tin Whiskers & Tin Pest

Tin WhiskersTin Whiskers are probably correctly are probably correctly seen as the greater evil, in that, they seen as the greater evil, in that, they occur in equipment operating under occur in equipment operating under normal conditions and can very easily normal conditions and can very easily cause short circuits in electronic hardware.cause short circuits in electronic hardware.

Tin PestTin Pest should not be ignored even should not be ignored even though it is thought to occur at very low though it is thought to occur at very low temperatures. Much of our hardware sees temperatures. Much of our hardware sees low temperatures, which is one reason low temperatures, which is one reason that we qualify electronic components that we qualify electronic components from -55 to +125.from -55 to +125.

Page 13: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

History Whisker FailuresHistory Whisker Failures During WW2 Cadmium whisker failures were During WW2 Cadmium whisker failures were

causing serious problems.causing serious problems. 1950’s Change to tin, resulted in same problems!1950’s Change to tin, resulted in same problems! The Whisker growth methodology still accepted The Whisker growth methodology still accepted

today was predicated in 1954.today was predicated in 1954. In 1975 a certain Mr. B.D. Dunn published the In 1975 a certain Mr. B.D. Dunn published the

Worlds 1Worlds 1stst paper containing high quality SEM paper containing high quality SEM micrographs of Whisker growth. He micrographs of Whisker growth. He recommended Srecommended SnnPPbb as the preferred finish for as the preferred finish for components.components.

Even in Commercial applications the US, NEMI Even in Commercial applications the US, NEMI state ”Pure Tin is unacceptable”.state ”Pure Tin is unacceptable”.

Page 14: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

History - Tin PestHistory - Tin Pest Tin Pest or Plague was known in the early 19Tin Pest or Plague was known in the early 19thth

Century and was, at one time credited with the Century and was, at one time credited with the French defeat in 1812, because the French tin French defeat in 1812, because the French tin uniform buttons literally disintegrated in the uniform buttons literally disintegrated in the extreme cold!extreme cold!

It was also blamed for the collapse of fuel cans It was also blamed for the collapse of fuel cans along Scott’s return route!along Scott’s return route!

The major problem that we face today is that The major problem that we face today is that under extreme cold conditions tin will disintegrate under extreme cold conditions tin will disintegrate as an insulator but become conductive if it warms as an insulator but become conductive if it warms up!up!

Page 15: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Minimisation of pure SMinimisation of pure Snn in in Spacecraft HardwareSpacecraft Hardware

The complete elimination of pure SThe complete elimination of pure Snn in Spacecraft Hardware is in Spacecraft Hardware is virtually impossible. However, Spur have become experts in virtually impossible. However, Spur have become experts in minimisingminimising its inclusion by:- its inclusion by:-

Careful control of Component Selection.Careful control of Component Selection. Detailed Component Assessment of non-qualified devices.Detailed Component Assessment of non-qualified devices. Specifying SSpecifying SnnPPbb whenever possible in Procurement Specs. whenever possible in Procurement Specs. Routinely carrying out lead / termination testing at R.I.Routinely carrying out lead / termination testing at R.I. Re-processing SMD SRe-processing SMD Snn components to inhibit whisker growth components to inhibit whisker growth Stripping and SStripping and SnnPPbb dipping of leaded components to dipping of leaded components to

minimise risk of whisker growthminimise risk of whisker growth

Even these precautions cannot guarantee pure SEven these precautions cannot guarantee pure Snn exclusion! exclusion!

Page 16: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Component Selection ControlComponent Selection Control Component Lists need to be reviewed for a wide range of Component Lists need to be reviewed for a wide range of

potential problems including:- Qualification , current and potential problems including:- Qualification , current and future availability & Quality history amongst others. future availability & Quality history amongst others.

However, with respect to Lead finish it is essential to:-However, with respect to Lead finish it is essential to:-

Maximise the use of components which are controlled by a Maximise the use of components which are controlled by a specification which offers Sspecification which offers SnnPPbb or A or Auu lead finish. lead finish.

Check that these components are still supplied in that Check that these components are still supplied in that finish, but don’t always expect a truthful answer from finish, but don’t always expect a truthful answer from stockists.stockists.

If pure SIf pure Snn is the only option offered then an alternative is the only option offered then an alternative component should be sought.component should be sought.

Where no alternative exists action must be taken to Where no alternative exists action must be taken to minimise the risks. minimise the risks.

Page 17: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Component AssessmentComponent Assessment Where no, or inadequate, previous knowledge of a Components Where no, or inadequate, previous knowledge of a Components

quality of assembly, is available, Component Assessment needs to quality of assembly, is available, Component Assessment needs to be carried out.be carried out.

WRT minimising SWRT minimising Snn it is natural to concentrate on the leads / it is natural to concentrate on the leads / terminations, but increasingly we are finding pure Sterminations, but increasingly we are finding pure Snn being used being used as an internal plating in cavity devices.as an internal plating in cavity devices.

Device found to have lid with pure tin finish

Page 18: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Sample component termination Sample component termination testingtesting

As a standard activity during Receiving Inspection, Lead / As a standard activity during Receiving Inspection, Lead / Termination EDAX Inspection is carried out as standard on a small Termination EDAX Inspection is carried out as standard on a small sample of all date codes.sample of all date codes.

Photos of EDAX SPhotos of EDAX Sn n & S& SnnPPbb

Page 19: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Re-processing pure SRe-processing pure Snn devices. devices. Spur have developed a means whereby Pure SSpur have developed a means whereby Pure Snn SMD’s can SMD’s can

be reprocessed such that the Pbe reprocessed such that the Pbb content exceeds 3% content exceeds 3% throughout the re-made joint, thus inhibiting whisker throughout the re-made joint, thus inhibiting whisker growth. growth.

pure tin re-processed jointpure tin re-processed joint

Page 20: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Spur process to mitigate pure tinSpur process to mitigate pure tin

1st re-flow showing pure tin remains on top of termination

Back Scatter image shows pure tin (no PPbb present) on top of termination

Page 21: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Spur process to mitigate pure tinSpur process to mitigate pure tin

2nd re-flow showing entire termination and solder fillet comprise of tin/lead mixture

Back Scatter image showing good amalgamation of tin and lead – even on top of termination

Page 22: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Stripping / TinningStripping / Tinning Most of us are aware of the process of stripping and Most of us are aware of the process of stripping and

reprocessing of pure Sreprocessing of pure Snn or A or Auu leaded components, and the leaded components, and the need to avoid overheating glass or ceramic body seals.need to avoid overheating glass or ceramic body seals.

The problem with SThe problem with SnnPPbb solder coated leads is that S solder coated leads is that Snn whiskers whiskers can still grow from the untreated area at the top of the lead.can still grow from the untreated area at the top of the lead.

Controlled Solder Dipping Process

•Pre-Heat Hot Plate

•IPA cleaner

•Flux

•De-Golding Pot

•Solder Dip Pot

•Controlled Immersion

Page 23: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Chemical StrippingChemical Stripping Spur believes that it has identified a means by Spur believes that it has identified a means by

which the entire lead can be chemically stripped which the entire lead can be chemically stripped of pure Sof pure Snn and can then be re-plated to within a and can then be re-plated to within a safe distance of the case.safe distance of the case.

The methodology needs to be assessed through a The methodology needs to be assessed through a properly controlled study managed by an properly controlled study managed by an accredited agency such as ESA.accredited agency such as ESA.

Spur would be prepared to offer its proposed Spur would be prepared to offer its proposed solution to its customers but unfortunately it has solution to its customers but unfortunately it has no evidence based results to demonstrate the no evidence based results to demonstrate the reliability of the procedure. reliability of the procedure.

Page 24: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

Space Grade Press Fit ConnectorsSpace Grade Press Fit Connectors EDX Analysis EDX Analysis

identified identified potentially potentially dangerous mix dangerous mix of termination of termination finishesfinishes

Page 25: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

SummarySummary

Tin Whiskers and Tin Pest have been known Tin Whiskers and Tin Pest have been known problems that remain with us.problems that remain with us.

In spite of the serious implications of banning SIn spite of the serious implications of banning SnnPPbb solders and finishes, Brussels has handed us a solders and finishes, Brussels has handed us a time bomb!time bomb!

Unless we are extremely vigilant we Unless we are extremely vigilant we willwill lose lose spacecraft to electrical failure caused by Sspacecraft to electrical failure caused by Snn related problems. related problems.

Page 26: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

SummarySummary

All of us involved in the design and manufacture All of us involved in the design and manufacture of Spacecraft hardware must ensure that we of Spacecraft hardware must ensure that we minimise the inclusion of Pure Tin within our minimise the inclusion of Pure Tin within our equipment, using the controls identified above.equipment, using the controls identified above.

We must also look for the means of removing SWe must also look for the means of removing Snn from our hardware to the maximum extent from our hardware to the maximum extent possible, using known inspection techniques and possible, using known inspection techniques and investigating new methods of removing the investigating new methods of removing the hazard that pure tin poses.hazard that pure tin poses.

Page 27: Elimination of S n in Spacecraft Assemblies Presentation to the EMAPS Workshop 17 th February 2010

End of showEnd of show

SPUR ELECTRON, UKSPUR ELECTRON, UKwww.spurelectron.comwww.spurelectron.com