Table of Contents Table of Contents
Previous Page  35 / 70 Next Page
Information
Show Menu
Previous Page 35 / 70 Next Page
Page Background

ple. The EDS map of the film acquired in the transmission

electron microscope shows a layer of silicon, oxygen, and

fluorine a few nm thick on this sample, similar to the

MoS

2

/Sb

2

O

3

/Au film. Because carbon erosion by AO results

in formation of volatile CO and CO

2

, the surface layer on

the DLN film is probably the result of both surface contam-

ination and the oxidized silicon that is naturally part of the

film remaining behind after erosion of the carbon phase.

Summary and outlook

Frictional behavior of solid lubricant films is highly in-

fluenced by phenomena that occur at the nanoscale. Sur-

face oxidation of just a few nanometers creates a

significantly higher initial friction coefficient for all MoS

2

films compared to the steady-state value, but lasts only a

few cycles until the oxidized layer is worn away. When slid-

ing in environments containing water vapor and oxygen,

dynamic oxidation and water vapor effects result in a

higher steady-state friction coefficient for MoS

2

films com-

pared to that exhibited in inert atmospheres or vacuum.

DLN films exhibit similar behavior to composite MoS

2

films, including a run-in period associated with removal

of surface contaminants and layers created by AO expo-

sure, as well as the development of a transfer film on the

mating surface.

Composite MoS

2

and DLN coatings have now been

flown in space to determine changes in surface composi-

tion and frictional behavior that accompany exposure to

AO in Low Earth Orbit. Samples exposed during MISSE-

7 experienced a fluence of AO about 14 times greater than

that during EOIM-3, but effects of LEO exposure on sur-

face chemistry and tribological behavior were very similar

for both missions. Given that oxide layers a few nm thick

are easily worn away exposing virgin lubricant underneath,

an intriguing possibility for protecting thin film solid lu-

bricants after deposition, but before use, may be to inten-

tionally cap the solid lubricant film with a layer of oxide or

metal to act as a barrier to the diffusion of water and oxy-

gen into the film.

For more information:

Michael T. Dugger and Somuri V.

Prasad, Materials Science and Engineering Center, Sandia Na-

tional Laboratories, Albuquerque, NM 87185-0889,

mt- dugge@sandia.gov

and

svprasa@sandia.gov

. T.W. Scharf is on

sabbatical from the Dept. of Materials Science and Engineer-

ing, The University of North Texas, Denton, TX 76203-5310.

Acknowledgments

The authors thank Paul Kotula for TEM analysis and

Andre Claudet for supporting the MISSE-7 tribological analy-

sis. MoS

2

/Sb

2

O

3

/Au and DLN coatings were provided by

Andy Korenyi-Both (Tribologix Inc.) and Chandra Venkatra-

man (Bekeart Advanced Coatings Technologies), respectively.

The MISSE-7 project for Sandia National Laboratories was

led by Gayle Thayer. Sandia National Laboratories (SNL) is a

multiprogram laboratory managed and operated by Sandia

Corp., a wholly owned subsidiary of Lockheed Martin Corp.,

for the U.S. DOE’s National Nuclear Security Administration

under Contract DE-AC04-94AL85000.

References

1. L. Leger, J. Visentine, and B. Santos-Mason, SelectedMaterials

Issues Associated with Space Station, 18th International SAMPE

Technical Conference 18, Oct. 7-9, 1986, Seattle.

2. M. Nicolet and P. Mange, The Dissociation of Oxygen in the

High Atmosphere,

J. Geophys. Res.,

Vol 59, p 15-45, 1954.

3. L. Leger and K. Dufrane, Space Station Lubrication Consider-

ations, Proc. 21st AMS, NASA Conf. Publ. 2470, 1987.

4. M.T. Dugger, Protective Coatings and Thin Films: Synthesis,

Characterization andApplications, Y. Pauleau and P.B. Barna, eds.,

NATO Advanced Research Workshop, May 30-June 5, 1996,

Alvor, Portugal, Klewer Academic Publishers, p 157-168, London,

1997.

5. M.R. Hilton and P.D. Fleischauer, Structural Studies of Sputter-

DepositedMoS

2

Solid Lubricant Films,Mat. Res. Soc. Symp. Proc.

140, p 227-238, 1990.

6. B.C. Stupp, Synergistic Effects of Metal Co-Sputtered with

MoS

2

,

Thin Solid Films,

Vol 84, p 257-266, 1981.

7. M.R. Hilton., et al., Structural and Tribological Studies of

MoS

2

Solid Lubricant Films Having Tailored Metal-Multilayer

Nanostructures,

Surf. Coat. Technol.,

Vol 53, p 13-23, 1992.

8. S.Y. Chung, et al., Flight- and Ground- Test Correlation Study

of BMDO SDSMaterials: Phase I Report, Jet Propulsion Labora-

tory, California Institute of Technology, Pasadena, CA (JPL Pub.

93-31), p 1-64, 1993.

9. T.W. Scharf, P.G. Kotula, and S.V. Prasad, Friction and Wear

Mechanisms inMoS

2

/Sb

2

O

3

/AuNanocomposite Coatings,

Acta

Mater.,

Vol 58, p 4100-4109, 2010.

10. T.W. Scharf, et al., Mechanisms of Friction in Diamondlike

Nanocomposite Coatings,

J. Appl. Phys.,

Vol 101, 063521-1, 2007.

ADVANCED MATERIALS & PROCESSES •

MAY 2014

35