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Journal of Surface Analysis Vol.13 No. 3 (2006) pp. 217 - 222 M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit - 217 - Copyright (c) 2006 by The Surface Analysis Society of Japan Characterization of Lubricative Coating after Exposure Test in Orbit M. Tosa a,* , A. Kasahara a , M. Goto a , Y. Pihosh a , S. Ota a , T. Kimura a , S. Fukushima a , T. Inoue b , E. Miyazaki b and K. Imagawa b a National Institute for Materials Science (NIMS) 1-2-1 Sengen, Tsukuba, Ibaraki 305-0047, Japan b Japan Aerospace Exploration Agency (JAXA) 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan * [email protected] (Received: April 25, 2006 ; Accepted: November 1, 2006) Change in such properties were characterized as tribological properties, surface chemical condition and so on for lubricative coating films of titanium nitride (TiN) that have been effected by exposure to an environment in orbit with the Russian Service Module / Space Environment Exposure Device (SM/SEED) prepared by JAXA on the International Space Station (ISS). Friction measurement with a mating pin of stainless steel showed that TiN coated stainless steel sheets after exposure test to orbit environment for a year generally decrease friction coefficient and can keep almost constant even after bakeout under a vacuum as well as at an atmospheric pressure due to some kind of modification of lubricant layer by the exposure. 1. Introduction Orbit environment of a space shuttle and a space station around the earth is known as an ultrahigh vacuum under 10 -5 Pa and usually suffers from atomic oxygen attack at a high speed as well as ultraviolet irradiation. Moving components materials therefore require surface modification with stable lubrication for preventing increase in friction force due to oxidation, irradiation damages and so on. We have prepared solid lubricative coating films of titanium nitride (TiN) on stainless steel sheets. TiN has advantages of combining the characteristic properties of covalent compounds, such as a high hardness and chemical and thermo-dynamical stability with metal-like electrical and thermal properties, which makes it a unique and excellent candidate in different technological areas [1]. Due to a low friction coefficient ( 0.17), TiN coating films are successfully utilized as surface protective coatings for tribological applications as well as sufficient diffusion barriers for metal interconnects in semiconductor devices [2-4]. TiN coated stainless steel sheets have been exposed on a space station in orbit for a year and then re- covered to the Earth. We have analyzed tribological proper- ties, surface chemical condition and so on in order to under- stand the change in properties of lubricant coating by expo- sure in orbit and also to develop advanced smooth and reli- able space solid lubricant coating. 2. Experimental Type 304 austenitic commercial stainless steel sheets (size; 14 mm×14 mm×1mm) have been coated with TiN using a radio frequency magnetron sputter deposition sys- tem with a film thickness about 500nm [5]. TiN coated stain- less steel sheets were set onto a panel as shown in Fig.1 and installed into the Russian Service Module / Space Environ- ment Exposure Device (SM/SEED) prepared by JAXA on the Russian service module in the International Space Sta- tion (ISS), and have been exposed in orbit then recovered to the Earth. Friction properties of TiN coated stainless steel sheets with and without exposure to orbit were observed with a system developed for measuring vacuum friction. Design of the friction measurement system comes from the Bowden-Leben type as shown in Fig.2 [6]. A sheet stage can move in x-y direction by two axes stepping motor and a manual axis in an ultrahigh vacuum. A sheet holder of an inch in diameter is easy to be fixed with plate spring. A ball pin prove above the sheet holder has a load weight holder with 0.49 N and has two strain gauges to detect frictional force. A mating pin made of stainless steel was scanned under normal load. The vacuum chamber including the fric- tion measurement system was evacuated with a tandem turbo-molecular pumping system and an iron pump down to 10 -5 Pa or less level. Surface chemical characterization for the sheets was carried out with a X-ray photoelectron spectros-

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Page 1: Characterization of Lubricative Coating after Exposure ... No.3/Vol... · M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit ... Characterization

Journal of Surface Analysis Vol.13 No. 3 (2006) pp. 217 - 222M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit

- 217 -

Copyright (c) 2006 by The Surface Analysis Society of Japan

Characterization of Lubricative Coating after ExposureTest in Orbit

M. Tosaa,*, A. Kasaharaa, M. Gotoa, Y. Pihosha, S. Otaa, T. Kimuraa, S. Fukushimaa,T. Inoueb, E. Miyazakib and K. Imagawab

aNational Institute for Materials Science (NIMS) 1-2-1 Sengen, Tsukuba, Ibaraki 305-0047, JapanbJapan Aerospace Exploration Agency (JAXA) 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan

*[email protected]

(Received: April 25, 2006 ; Accepted: November 1, 2006)

Change in such properties were characterized as tribological properties, surface chemical condition and so onfor lubricative coating films of titanium nitride (TiN) that have been effected by exposure to an environment inorbit with the Russian Service Module / Space Environment Exposure Device (SM/SEED) prepared by JAXA onthe International Space Station (ISS). Friction measurement with a mating pin of stainless steel showed that TiNcoated stainless steel sheets after exposure test to orbit environment for a year generally decrease frictioncoefficient and can keep almost constant even after bakeout under a vacuum as well as at an atmosphericpressure due to some kind of modification of lubricant layer by the exposure.

1. IntroductionOrbit environment of a space shuttle and a space station

around the earth is known as an ultrahigh vacuum under10-5 Pa and usually suffers from atomic oxygen attack at a highspeed as well as ultraviolet irradiation. Moving componentsmaterials therefore require surface modification with stablelubrication for preventing increase in friction force due tooxidation, irradiation damages and so on. We have preparedsolid lubricative coating films of titanium nitride (TiN) onstainless steel sheets. TiN has advantages of combining thecharacteristic properties of covalent compounds, such as ahigh hardness and chemical and thermo-dynamical stabilitywith metal-like electrical and thermal properties, which makesit a unique and excellent candidate in different technologicalareas [1]. Due to a low friction coefficient ( ~0.17), TiNcoating films are successfully utilized as surface protectivecoatings for tribological applications as well as sufficientdiffusion barriers for metal interconnects in semiconductordevices [2-4]. TiN coated stainless steel sheets have beenexposed on a space station in orbit for a year and then re-covered to the Earth. We have analyzed tribological proper-ties, surface chemical condition and so on in order to under-stand the change in properties of lubricant coating by expo-sure in orbit and also to develop advanced smooth and reli-able space solid lubricant coating.

2. ExperimentalType 304 austenitic commercial stainless steel sheets

(size; 14 mm×14 mm×1mm) have been coated with TiNusing a radio frequency magnetron sputter deposition sys-tem with a film thickness about 500nm [5]. TiN coated stain-less steel sheets were set onto a panel as shown in Fig.1 andinstalled into the Russian Service Module / Space Environ-ment Exposure Device (SM/SEED) prepared by JAXA onthe Russian service module in the International Space Sta-tion (ISS), and have been exposed in orbit then recovered tothe Earth. Friction properties of TiN coated stainless steelsheets with and without exposure to orbit were observedwith a system developed for measuring vacuum friction.Design of the friction measurement system comes from theBowden-Leben type as shown in Fig.2 [6]. A sheet stage canmove in x-y direction by two axes stepping motor and amanual axis in an ultrahigh vacuum. A sheet holder of aninch in diameter is easy to be fixed with plate spring. A ballpin prove above the sheet holder has a load weight holderwith 0.49 N and has two strain gauges to detect frictionalforce. A mating pin made of stainless steel was scannedunder normal load. The vacuum chamber including the fric-tion measurement system was evacuated with a tandemturbo-molecular pumping system and an iron pump down to10-5 Pa or less level. Surface chemical characterization for thesheets was carried out with a X-ray photoelectron spectros-

Page 2: Characterization of Lubricative Coating after Exposure ... No.3/Vol... · M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit ... Characterization

Journal of Surface Analysis Vol.13 No. 3 (2006) pp. 217 - 222M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit

- 218 -

copy using a PHIエs Quantera SXM with X-ray of excited fromAl K (1486.6 eV), constant pass energy of 69 eV, X-ray beamsize of 100 m in diameter and so on.

3. Results and Discussion3. 1. Friction PropertiesFriction properties of the TiN coated stainless steel sheets

sliding against stainless steel as exposure test sheets weredetermined both at an atmospheric pressure and in an ultra-high vacuum. TiN coated stainless steel sheet shows a fric-tion coefficient ( ) of 0.12 at an atmospheric pressure andshows an increased value of 0.26 in 10-5 Pa. TiN coatedstainless steel sheet after exposure test in orbit for a yearshows a low friction coefficient of 0.10 at an atmosphericpressure and shows a small increased value of 0.11 in 10-5

Pa. It might be considered that TiN coated stainless steelsheets with exposure to orbit environment generally de-

Fig.1 Photo of a panel with attached TiN coated stainless steelsheets for SM/SEED module.

Fig.2 Schematic view of a vacuum friction measurement systemand photo of a center system.

crease friction coefficient under a vacuum of 10-5 Pa as wellas at an atmospheric pressure due to atomic oxygen attackand ultraviolet irradiation. Fig.3 shows change in a frictionforce of TiN coated stainless steel sheets with and withoutexposure as changing normal load. The exposed TiN coatedstainless steel sheet shows a little bit of higher friction thanno exposed TiN stainless steel sheet under low normal load.This might be due to an increase in adsorption force bychange in surface roughness on a nano-scale.We have also measured the friction coefficient of TiN

coated stainless steel sheets after exposure in orbit in orderto estimate the thermal stability by vacuum annealing. Fig.4shows a change in a friction coefficient ( ) of TiN coatedstainless steel sheet with exposure at an ambient tempera-ture about 300 K to have been kept and measured in situafter annealing at 500 K in an ultrahigh vacuum about 10-5

Pa. Little change in friction coefficients of TiN coated stain-less steel sheet exposed in orbit after vacuum annealing isshown and such thermal stability might come from forma-tion of tough coating layer independent of adhesion layerwith good effect on friction.

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Journal of Surface Analysis Vol.13 No. 3 (2006) pp. 217 - 222M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit

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Fig.3 Change in a friction force of TiN coated stainless steel sheetswith and without exposure as changing normal load.

Fig.4 Change in a friction coefficient ( ) of TiN coated stainlesssteel sheet with exposure after annealing at 500K in a vacuum.

Fig.5 Survey spectra of exposed (A) and screened area (B) of TiNcoated stainless steel sheets.

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Journal of Surface Analysis Vol.13 No. 3 (2006) pp. 217 - 222M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit

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3. 2. Surface AnalysesSurface chemical condition and depth profile were ob-

tained with a X-ray photoelectron spectroscopy for two ar-eas of TiN coated stainless steel sheets, one for exposureand the other for screening against exposure in orbit. Fig.5shows survey spectra of exposed and screened stainlesssteel sheets coated with TiN. Silicon (Si) peaks and largeoxygen (O) peaks are observed on the exposed area whilelarge fluorine (F) peaks are observed on screened area of theTiN coated stainless steel sheet. Fig.6 shows depth profilesof exposed and screened area of the stainless steel sheetcoated with TiN. Silicon and oxygen concentrated layer isobserved at the surface of TiN coating layer at the exposedarea in orbit.Changes in chemical condition were obtained for elements

composing TiN coated stainless steel sheets after exposurein orbit as shown in Fig.7 with main binding energies [7].Titanium forms TiN with nitrogen mainly and also formsTiO2 with oxygen in part. Silicon forms SiO2 with oxygen at thesurface of TiN coating layer.Comparison between these surface analytical results of

exposed and screened area of TiN coated stainless steelsheet indicates as follows. TiOx layer formed during TiN filmpreparation. Silicon evaporated from silicone adhesives usedfor space station structure might react the atomic oxygen toform SiO2 during exposure in orbit. The mixed structure ofSiO2 in coating film is considered to form a good lubricantlayer that can offer smooth and stable sliding against an-nealing in a vacuum.

4. ConclusionsTiN coated stainless steel sheets were prepared with a

radio frequency sputtering deposition and then installedinto SM/SEED in orbit for a year. Results obtained with thefriction measurement system using a mating pin of stainlesssteel and X-ray photoelectron spectroscopy showed thatTiN coated stainless steel sheets with exposure to orbit en-vironment for a year decreased friction coefficient and couldkeep almost constant even after annealing in a vacuum aswell as at an atmospheric pressure due to some kind of oxi-dation of lubricant layer especially consisting of silicon ox-ide during the exposure. TiN coating will be therefore one ofgood candidates for space lubricative modification of mov-ing materials and oxidization of TiN with mixed silicon oxidemight lead to new lubricant material for tough environments.

Fig.6 Depth profiles of exposed (A) and screened area (B) of TiNcoated stainless steel sheets.

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Journal of Surface Analysis Vol.13 No. 3 (2006) pp. 217 - 222M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit

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Sputter time (min)

N1s

N1s (TiN): 396.9 eV

Sputter time (m

in)

Ti2p3/2 (TiO2): 458.8 eV

Ti2p3/2 (TiN): 455.8 eV

Ti2p

Fig.7 Changes in XPS spectra for main elements with sputter time for obtaining depth profile.

Fe2p

Fe2p3/2 (Fe): 707.0 eV

Sputter time (min)

Sputter time (min)

Si2p

Si2p (SiO2): 103.3 eV

Sputter time (min)

O1s

O1s (SiO2): 533.0 eV O1s (TiO2): 529.9 eV

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Journal of Surface Analysis Vol.13 No. 3 (2006) pp. 217 - 222M. Tosa et al. Characterization of Lubricative Coating after Exposure Test in Orbit

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ReferencesJ. E. Sundgren, Thin Solid Films 128, 21 (1985) .J. S. Chun, I. Petrov, and J. E. Greene, J. Appl. Phys. 86,3633(1999).M. Stoiber, E. Badisch, C. Lugmair, C. Mitterer, Surf.Coat. Technol. 163, 451 (2003).S. Ikeda, J. Palleau, J. Torres, B. Chenevier, N. Bourhila,and R. Madar, J. Appl. Phys. 86, 2300 (1999).M. Goto, A. Kasahara, M. Tosa, J. Hobley, M. Kishimoto,K. Yoshihara and H. Fukumura, J. Vac. Sci. and Technol.A20, 1458 (2002).A. Kasahara, M. Goto, M. Tosa and K. Yoshihara, J.Electroanalytical Chemistry 45, 559(2003).J. Chastain and R. C. King, Jr., Handbook of X-rayPhotoelectron Spectroscopy, Physical Electronics Inc.,Minnesota (1995).

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