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DTIC ADA503737: Protection of Polymer from Atomic-Oxygen Erosion using Al2O3 Atomic Layer Deposition Coatings PDF

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Preview DTIC ADA503737: Protection of Polymer from Atomic-Oxygen Erosion using Al2O3 Atomic Layer Deposition Coatings

Available online at www.sciencedirect.com ThinSolidFilms516(2008)4036–4039 www.elsevier.com/locate/tsf Letter Protection of polymer from atomic-oxygen erosion using Al O atomic layer 2 3 deposition coatings ⁎ Russell Coopera, Hari P. Upadhyayaa, Timothy K. Minton a, , Michael R. Berman b, Xiaohua Duc, Steven M. Georgec a DepartmentofChemistryandBiochemistry,MontanaStateUniversity,Bozeman,MT59717,USA bAirForceOfficeofScientificResearch,875N.RandolphStreet,Arlington,VA22203,USA c DepartmentsofChemistryandBiochemistryandChemicalandBiologicalEngineering,UniversityofColorado,Boulder,CO80309,USA Received8April2007;receivedinrevisedform2July2007;accepted13July2007 Availableonline21July2007 Abstract ThinfilmsofAl O grownusingatomiclayerdeposition(ALD)techniquescanprotectpolymersfromerosionbyoxygenatoms.Toquantify 2 3 thisprotection,polyimidesubstrateswiththesamechemicalrepeatunitasKapton®wereappliedtoquartzcrystalmicrobalance(QCM)sensors. Al O ALDfilmswithvaryingthicknessesweregrownonthepolyimidesubstrates.TheALD-coatedpolyimidematerialswerethenexposedtoa 2 3 hyperthermal atomic-oxygen beam. The mass loss versus oxygen-atom exposure time was measured in situ by the QCM. Al O ALD film 2 3 thicknesses of ∼35Å werefoundto protect the polymer fromerosion. ©2007Elsevier B.V. All rightsreserved. Keywords:Polymers;Polyimide;Ätomiclayerdeposition;Al2O3;Atomicoxygen;Erosion;Quartzcrystalmicrobalance Spacecraft in low Earth orbit collide with ambient oxygen However,handlingandthermalcyclingofthesethickcoatingsare atomswithrelativevelocitiesof∼7.4kms−1andfluxesinthe likelytoproducecracksinthecoatingsandexposethesubstrateto range of 1013 to 1015 atoms cm−2 s−1. These high-energy potentialO-atomattack.Atomicoxygenthatreachesthesubstrate collisions cause oxidation and erosion of materials. Organic throughdefectsmayerodelargecavitiesunderneaththecoatingin polymers used on the external surfaces of spacecraft as thevicinityofthedefect[6,7]. structuralandthermal-controlmaterialsareparticularlyvulner- ThePECVDcoatingtechniquealsorequiresline-of-sightto abletoatomicoxygen[1–4].Coatingsofinorganicoxides,such thesubstrate.Thisrequirementmaybeimpracticalforshadowed as SiO , have been used to provide protection from atomic or high-aspect-ratio structures. An approach that is an 2 oxygen. These coatings are generally applied by plasma improvement over PECVD is to attach silicon-containing enhanced chemical vapor deposition(PECVD). moieties to the surface through a photochemical reaction. The PECVD is known to produce films that tend to be columnar modifiedsurfacemaythenreactwithatomicoxygentoforma withalargedefectdensity.Becauseofthelargenumberofdefects, continuous layer of SiO . Although this technique has 2 relatively thick coatings have been used to reduce the defect demonstratedaonehundred-foldreductioninerosionyieldfor density.Kapton®polyimidesurfacesthathaveSiO coatingswitha flat samples, there are still line-of-sight limitations when the 2 1300Åthicknesshavebeenshowntoexhibiterosionyieldsaslow techniqueisappliedtonon-planarsurfaces[8]. as∼0.1–0.2%oftheerosionyieldofunprotectedKapton®[5,6]. In addition to protecting existing polymers with inorganic coatings, inorganic/organic copolymers are being developed thattakeadvantageofthereactionoftheinorganiccomponent ⁎ Correspondingauthor. with atomic oxygen to form a passivating oxide layer. This E-mailaddresses:[email protected](T.K.Minton), protection strategy has the advantage that the oxide layer can [email protected](M.R.Berman),[email protected] (S.M.George). reformafterthedegradationoftheinitialoxidelayer.Anearlier 0040-6090/$-seefrontmatter©2007ElsevierB.V.Allrightsreserved. doi:10.1016/j.tsf.2007.07.150 Report Documentation Page Form Approved OMB No. 0704-0188 Public reporting burden for the collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to a penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. 1. REPORT DATE 3. DATES COVERED 02 JUL 2007 2. REPORT TYPE 00-00-2007 to 00-00-2007 4. TITLE AND SUBTITLE 5a. CONTRACT NUMBER Protection of polymer from atomic-oxygen erosion using Al2O3 atomic 5b. GRANT NUMBER layer deposition coatings 5c. PROGRAM ELEMENT NUMBER 6. AUTHOR(S) 5d. PROJECT NUMBER 5e. TASK NUMBER 5f. WORK UNIT NUMBER 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION University of Colorado,Department of Chemistry and REPORT NUMBER Biochemistry,Boulder,CO,80309 9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSOR/MONITOR’S ACRONYM(S) 11. SPONSOR/MONITOR’S REPORT NUMBER(S) 12. DISTRIBUTION/AVAILABILITY STATEMENT Approved for public release; distribution unlimited 13. SUPPLEMENTARY NOTES 14. ABSTRACT see report 15. SUBJECT TERMS 16. SECURITY CLASSIFICATION OF: 17. LIMITATION OF 18. NUMBER 19a. NAME OF ABSTRACT OF PAGES RESPONSIBLE PERSON a. REPORT b. ABSTRACT c. THIS PAGE Same as 4 unclassified unclassified unclassified Report (SAR) Standard Form 298 (Rev. 8-98) Prescribed by ANSI Std Z39-18 R.Cooperetal./ThinSolidFilms516(2008)4036–4039 4037 class of self-passivating polymers was based on phosphine Aluminum oxide (Al O ) ALD coatings with various 2 3 oxide [9]. More recently, copolymers that include polyoligo- thicknesses were applied to the polyimide substrates using meric silsesquioxane have shown great promise as a replace- sequential, self-limiting exposures to trimethylaluminum mentforKapton® [10].However,thesepolymersexhibitfinite (TMA) (Aldrich) and water (Fisher HPLC-grade). The Al O 2 3 erosion by atomic oxygen and may experience damage under ALDwasperformedat177°Cinaviscousflow,hot-wallALD vacuum ultraviolet (VUV) radiation inspace. flow reactor [25]. The TMA and H O yield Al O ALD 2 2 3 Earlierstudiesindicatethatanultrathinandflexibleinorganic accordingtothefollowingtworeactions[18,19]: oxide coating may provide an effective barrier. Exposure of a ⁎ ⁎ siliconsurfacetoabeamofhyperthermalatomicoxygenleadsto ðAÞAl–OH þAlðCH Þ →Al–O–AlðCH Þ þCH ð1Þ thegrowthofanSiO filmwithaterminalthicknessof∼50Å 3 3 3 2 4 2 [11–13]. The native thickness of aluminum oxide (Al O ) on ⁎ ⁎ 2 3 ðBÞAl–CH þH O→Al–OH þCH ð2Þ aluminum has also been measured to be only 30–40 Å [14]. 3 2 4 Anecdotalevidencefromspaceflightexperimentsexiststhatan wheretheasterisksdenotethesurfacespecies.Whenperformed Al2O3 coating with a nominal thickness of 50 Å protects a in an ABAB… reaction sequence, these sequential reactions reactivesubstrate [15].Ifsuchthin andflexible oxide coatings produce linear, atomic-layer-controlled Al O growth. The 2 3 can be applied to polymer substrates without line-of-sight steady-state Al O ALD growth rate after nucleation is 2 3 restrictions and without defects, then they should be able to ∼1.2 Å per AB cycle [19,26]. The polyimide substrates were protectthesubstrateevenafterhandlingandthermalcycling. coated with Al O ALD films resulting from 8, 13, 17, 21, 25 2 3 Chemicalvapordeposition(CVD)isawellcharacterizedthin and50ABcycles,respectively.Thereactantexposuresequence film deposition method that does not depend on line-of-sight. wasTMA(1.0s),purge(20s),H O(1.0s),andpurge(10s).The 2 However, CVD methods typically require elevated substrate polyimide surfaces were coated without any prior surface temperatures togrow the desired films. Avariation on CVD is treatmentorfunctionalization. atomiclayerdeposition(ALD).ALDcanusuallyemploymore ThecoatedQCMsensorswereexposedtoabeamcontaining reactiveprecursorgasesthanCVDandachievelowerdeposition hyperthermal atomic oxygen. Mass loss was measured in situ temperatures. ALD techniques can also produce continuous, versustimeusingaMaxtekQCMhead(ModelDSH-200)anda Angstrom-level-controlled,anddefect-freefilms[16].ALDisa Model RQCM data collection system. The QCM head accom- gas-phasemethodbasedontwosequential,self-limitingsurface modatedtwodiscs,allowingeachatomic-oxygenexposuretobe reactions[17].Eachsurfacereactionallowsonly∼1monolayer conducted with an Al O -coated polyimide test sample and a 2 3 ofdeposition. polyimide control sample without an Al O coating. For each 2 3 Al O ALD is a particularly robust and well-defined ALD 2 3 exposure,theatomic-oxygenfluxwasdeterminedfromthemass- system [18,19]. Al O ALD films can be pinhole-free as 2 3 lossrateofthepolyimidecontrolsample.Theoxygen-atomflux demonstratedbyelectricalmeasurements[20],andtheycanbe did not vary by more than a few percent from one exposure to depositedonpolymersubstrates[21,22].Excellentgasdiffusion another.Testandcontrolsampleswerealwaysplacedinthesame barrier properties are observed for Al O ALD films on 2 3 locationstoensureconsistencybetweenthevariousexposures. polyethylene naphthalate (PEN) and Kapton® polymer sub- A pictorial diagram of the atomic-oxygen source and strates [23,24]. Consequently, Al O ALD should provide an 2 3 experimental apparatus is shown in Fig. 1. This apparatus has idealmodelsystemforthesystematicinvestigationofthin-film coatingstoprotectapolymerfromhyperthermalatomicoxygen. Quartz crystal microbalance (QCM) sensors were used to studytheefficacyofthinAl O ALDfilmstoprotectapolymer. 2 3 Polyimidesubstrateswerepreparedon0.5-inch-diameterQCM disc sensors. The precursor to the polyimide was Pyralin® PI5878G from HD Microsystems. This polyamic acid as pur- chased was dissolved in 1-methyl-2-pyrrolidinone. The polya- mic acid was diluted and then spin-coated onto gold-coated QCM sensors. Before spin-coating, the QCM sensors were modifiedbyapplyinganadhesionpromoter(HDMicrosystems VM651) and heating the substrates in an air oven to 80 °C to removeanyresidualwater.Afterspin-coating,thesampleswere allowed to dry in air under a watch glass for two days. The sampleswerethenplacedinavacuumfurnace(CenturionVPM) andcuredwiththefollowingschedule:2hat50°C,2hat80°C, 1 h at 200 °C, and 2 h at 270 °C. The chemical repeat unit of theresultingpolyimideisequivalenttothatofDuPontKapton®. ThepolyimidelayersontheQCMdiscsensorsweredetermined Fig.1.Experimental apparatususedtomeasurethemasslossof spin-coated by profilometry to have thicknesses in the range of 800– polyimidelayersonQCMsensorsduringexposuretoahyperthermalatomic- 1000nm. oxygenbeam. 4038 R.Cooperetal./ThinSolidFilms516(2008)4036–4039 Theerosionofpolymersubstratesbyanoxygenplasmainthe vicinity of coating defects has previously been used to make defectsmorevisibletoSEMandopticalinspection[30].Defects intheALDcoatingswouldbeexpectedtobesimilarlyamplified by exposure to the hyperthermal O-atom beam. Scanning electron microscope (SEM) images of the exposed surfaces showed erosion that was consistent with the mass loss measurements. The SEM images also demonstrated the sensitivity of the QCM to identify mass loss from erosion at tinydefectsonthesurface. Fig. 3 shows SEM imagesfor exposed surfaces with Al O 2 3 ALD films after 17, 21 and 50 AB cycles for atomic oxygen exposuretimesof500min.Theleftandrightcolumnsconsistof images collected with low (×20) and high (×1000) magnifica- Fig.2.Masschangeofpolyimidesubstratescoatedwithvaryingnumbersof tion, respectively. The number and size of defects decrease as Al2O3ALDABcyclesversusexposuretimetoatomicoxygen. the number of AB cycles increases. The surface after 17 AB cycles exhibits numerous large round defects that appear as been described in detail previously [1,10,27,28]. Sample regions where the polymer substrate has eroded significantly. exposures were performed with a pulsed beam operating at a Thesurfaceafter21ABcycleshasmanysmalldefectsscattered repetitionrateof2Hz.Thepulsedbeamcontainedhyperthermal overthesurface.Thesurfaceafter50ABcyclesdoesnotshow O(3P)atomsandO moleculesthatweregeneratedwithalaser- anydefects that can berelatedto theatomic-oxygen exposure. 2 breakdown source [28,29]. Average translational energies for The Al O ALD films after 8, 13, 17 and 21 ABcycles are 2 3 atomic and molecular oxygen were ∼5.4 and ∼9.3 eV, poorprotectingbarriersagainstattackbyoxygenatoms.Earlier respectively.Theenergywidths(fullwidthathalfmaximum)of QCM and X-ray fluorescence measurements revealed that the atomic and molecular oxygen components were ∼2.0 and approximately 10–20 AB cycles are required to nucleate a ∼5.3 eV, respectively. The average mole fraction of atomic continuous Al O film on various polymer substrates [22,31]. 2 3 oxygeninthebeamwas∼90%. Prior to nucleation, the ALD reactants are observed by QCM ThehyperthermalO-atombeamwasdirectedatthepolymer measurementstoabsorbintothepolymer[22].Afternucleation, samples on QCM sensors that were positioned about 40 cm anAl O ALDfilmbarriercontinuouslycoversthepolymerand 2 3 fromtheapexoftheconicalnozzle.Masslossasafunctionof blocksanyreactantabsorptionintothepolymer. time for both the test and control samples was recorded for at least 500 min. This time corresponds to 60,000 pulses of the hyperthermalbeamforeachatomic-oxygenexposure.Basedon the erosion yield of a Kapton® H polyimide [27], the atomic- oxygen flux was ∼2×1015 O atoms cm−2 pulse−1. Mass loss results for Al O ALD film thicknesses resulting 2 3 from8,13,17,21,25and50ABcyclesareshowninFig.2.The uncoated polyimide control sample eroded away completely duringeveryexperiment.Thelinearmasslossrateforthecontrol samplewasconsistentwithalossof600μgcm−2after500min. Polyimide samples with Al O ALD films after 8 and 13 AB 2 3 cycleserodedbefore500minofexposure.Thesamplewithan Al O ALDfilmafter17ABcycles showedarapid changeof 2 3 slopeafter300minofexposureandprobablywouldhaveeroded completelyiftheexposurehadsignificantlyexceeded500min. The samples with Al O ALD films after 21 and 25 AB 2 3 cyclesshowedaverygraduallossofmassduringtheexposure. Themasslossforthesampleafter25ABcyclesisonlyslightly higherthanthemasslossexpectedwhenoxygenatomsremove residualcontaminationfromthesurface.Thepolyimidesample coated with an Al O ALD film after 50 AB cycles did not 2 3 exhibitanymeasurablemasschangeaftermorethan500minof exposure. This Al O ALD film presumably has no defects or 2 3 pinholes where O atoms could attack the polyimide substrate. The measurements suggest a threshold of ≥25 AB cycles for Fig.3.SEMimagesofpolyimidesubstratescoatedwith17,21,and50Al O Al O ALD coatings to protect a polymer substrate from 2 3 2 3 ALDABcyclesafterexposuretoatomicoxygen.Theleftandrightcolumns erosion by oxygen atoms with ∼5 eVof translational energy. displayimagescollectedwith×20and×1000magnification,respectively. R.Cooperetal./ThinSolidFilms516(2008)4036–4039 4039 Theabsenceofdefectsonthepolyimidesampleafter50AB [2] E.Murad,J.Spacecr,Rockets33(1996)131. cycles of Al O ALD is consistent with the observation of no [3] L.E.Murr,W.H.Kinard,Am.Sci.81(1993)152. 2 3 [4] R.C.Tennyson,Can.J.Phys.69(1991)1190. mass loss during atomic-oxygen exposure. This Al O ALD 2 3 [5] S.K. Rutledge, J.A. Mihelic, in: V. Srinivasan, B.A. Banks (Eds.), filmisanexcellentprotectinglayerforthepolyimidesubstrate. MaterialsDegradationinLowEarthOrbit(LEO),TheMinerals,Metals& The thin Al2O3 ALD film after 50 AB cycles should have an MaterialsSociety,1990,p.35. Al O ALD film thickness on top of the polymer surface of [6] S.K. Rutledge, R.M. Olle, 38th International SAMPE Symposium, 2 3 ∼35Å.ThisestimatedthicknessassumesthattheAl O ALD May10–13,1993Covina,CA,Int.SAMPESYmp.Exhib.,vol.38,1993, 2 3 p.679. film requires 20 AB cycles to nucleate on the polyimide [7] B.A.Banks,A.Snyder,S.K.Miller,K.K.deGroh,R.Demko,J.Spacecr, substrate [22,31]. Rockets41(2004)335. TheAl2O3ALDthicknessof∼35Årequiredtoprotectthe [8] J.I.Kleiman,Mater.Res.Soc.Symp.Proc.851(2005)343. polyimide can be compared with the native oxide thickness of [9] J.W.Connell,J.G.Smith,J.L.Hendrick,Polymer36(1995)13. 30–40 Å on aluminum nanoparticles [14]. This native oxide [10] A.L. Brunsvold, T.K. Minton, I. Gouzman, E. Grossman, R. Gonzalez, HighPerform.Polym.16(2004)303. thickness serves as barrier to prevent additional aluminum [11] M.Tagawa,T.Ema,H.Kinoshita,N.Ohmae,M.Umeno,T.K.Minton, oxidation.Earliermeasurementsofthewatervaportransmission Jpn.J.Appl.Phys.,Part237(1988)L1455. rate through Al2O3 ALD films on PEN and Kapton® also [12] M.Tagawa,K.Yokota,N.Ohmae,H.Kinoshita,HighPerform.Polym.12 measuredextremelylowtransmissionratesforAl O ALDfilm (2000)53. 2 3 thicknesses N50 Å [24]. The H O permeability is believed to [13] M.Kisa,T.K.Minton,J.C.Yang,J.Appl.Phys.97(2005)023520. 2 [14] C.E.Aumann,G.L.Skofronick,J.A.Martin,J.Vac.Sci.Technol.,B13 be dominated by defects [32]. Analogous behavior may be (1995)1178. occurring for atomic oxygen penetration through the Al O 2 3 [15] S.Y.Chung,D.E.Brinza,T.K.Minton,A.E.Stiegman,J.T.Kenny,R.H. ALDfilms. Liang, JPL Publication 93-91 (Prepared for the Ballistic Defense ComparisonoftheAl O ALDthicknessof∼35Åwiththe Organization by the Jet Propulsion Laboratory, California Institute of 2 3 SiO filmthicknessof∼50Åformedbyoxidationofsiliconin Technology,Pasadena,CA.,1993). 2 a hyperthermal atomic oxygen beam [11–13] suggests that [16] T.Suntola,ThinSolidFilms216(1992)84. [17] S.M.George,A.W.Ott,J.W.Klaus,J.Phys.Chem.100(1996)13121. Al O is more effective at blocking hyperthermal O atoms. 2 3 [18] A.C.Dillon,A.W.Ott,J.D.Way,S.M.George,Surf.Sci.322(1995)230. Al2O3 ALD films can be deposited on polymers of any [19] A.W.Ott,J.W.Klaus,J.M.Johnson,S.M.George,ThinSolidFilms292 geometry. The Al O ALD films should also remain flexible (1997)135. 2 3 anduncompromisedifthepolymerisbentduringhandlingor [20] M.D.Groner,J.W.Elam,F.H.Fabreguette,S.M.George,ThinSolidFilms 413(2002)186. if the polymer expands and contracts during thermal cycling. [21] J.D.Ferguson,A.W.Weimer,S.M.George,Chem.Mater.16(2004)5602. TheAl O ALDfilmswithathicknessof35Åweredeposited 2 3 [22] C.A.Wilson,R.K.Grubbs,S.M.George,Chem.Mater.17(2005)5625. with 50 AB cycles with each cycle requiring approximately [23] P.F.Carcia,R.S.McLean,M.H.Reilly,M.D.Groner,S.M.George,Appl. 32s.Thetimerequiredtodepositthisfilmcouldbeshortened Phys.Lett.89(2006)031915. considerablywiththeuseofanoptimizedreactordesign.The [24] M.D.Groner,S.M.George,R.S.McLean,P.F.Carcia,Appl.Phys.Lett.88 (2006)051907. ALD method may also be used to apply oxide coatings other [25] J.W.Elam,M.D.Groner,S.M.George,Rev.Sci.Instrum.73(2002)2981. than Al O . Multilayer ALD films of Al O /TiO or Al O / 2 3 2 3 2 2 3 [26] M.D.Groner,F.H.Fabreguette,J.W.Elam,S.M.George,Chem.Mater.16 ZnO could protect against both O atoms and VUV light. (2004)639. [27] D.M. Buczala, A.L. Brunsvold, T.K. Minton, J. Spacecr. Rockets 43 Acknowledgement (2006)421. [28] D.J. Garton, A.L. Brunsvold, T.K. Minton, D. Troya, B. Maiti, G.C. Schatz,J.Phys.Chem.,A110(2006)1327. ThisworkwassupportedbytheAirForceOfficeofScientific [29] G.E.Caledonia,R.H.Krech,B.D.Green,AIAAJ.25(1987)59. Research(FA9550-04-1-0428andFA9550-06-1-0075). [30] A.S.daSilvaSobrinho,G.Czeremuszkin,M.Latrèche,G.Dennler,M.R. Wertheimer,Surf.Coat.Technol.116-119(1999)1204. References [31] J.W.Elam,C.A.Wilson,M.Schuisky,Z.A.Sechrist,S.M.George,J.Vac. Sci.Technol.,B21(2003)1099. [32] G.L.Graff,R.E.Williford,P.E.Burrows,J.Appl.Phys.96(2004)1840. [1] T.K.Minton,D.J.Garton,in:R.A.Dressler(Ed.),ChemicalDynamicsin ExtremeEnvironments,AdvancedSeriesinPhysicalChemistry,vol.11, WorldScientific,Singapore,2001,p.420.

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