Friction Reducing Composite Plating in Rocket Launchers
Year 2017,
Volume: 9 Issue: 3, 1 - 5, 26.12.2017
Ebru Saraloğlu Güler
,
İshak Karakaya
Abstract
Composite plating is commonly used for reducing
friction and wear. It is a method that can be used in the environments exposed
to friction such as rocket launchers. Steel specimens were coated by nickel
including MoS2 particles in this study. The effects of MoS2 particle
concentration and particle size on the coefficient of friction and the amount
of wear were determined by pin on disc tribometer. It is revealed that the
particles with small size and high concentration are more effective in
decreasing the friction coefficient.
References
- ASTM-G99-95a (2000), Standard Test Method for Wear Testing with a Pin-on-Disk Apparatus, ASTM International.
- Cardinal, M.F., Castro, P.A., Baxi J., Liang, H., Williams, F.J. (2009). Characterization and frictional behavior of nanostructured Ni-W-MoS2 composite coatings. Surface and Coatings Technology, 204(1-2), 85-90.
- Charles, J., Barker, L. and Kern, W. K. (1963). Aircraft rocket launcher US 3077144 A
- Hilton, M.R. and Fleischauer,P.D. (1992). Applications of Solid Lubricant Films in Spacecraft. Surface and Coating Technology, 54-55, 435-441.
- Hou, K.-H., Wang, H.-T., Sheu, H.-H. and Ger, M.-D. (2014). Preparation and wear resistance of electrodeposited Ni–W/diamond composite coatings. Applied Surface Science, 308, 372–379.
- Huang, Z.-j. and Xiong D.-s. (2008). MoS2 coated with Al2O3 for Ni-MoS2/Al2O3 composite coatings by pulse electrodeposition. Surface and Coatings Technology, 202(14), 3208-3214.
- Saraloglu Guler, E., İ. Karakaya, and E. Konca (2013). Effect of Electrodeposition Parameters on the Current Density of Hydrogen Evolution Reaction in Ni and Ni-MoS2 Composite Coatings. Int. J. Electrochem. Sci., 8, 5496 - 5505.
- Siopis, M.J. and Cowan, R.S. (2014). Electromagnetic Launch Technology (EML). International Symposium on Electromagnetic Launch Technology, 7-11 July, San Diego, 865.
Year 2017,
Volume: 9 Issue: 3, 1 - 5, 26.12.2017
Ebru Saraloğlu Güler
,
İshak Karakaya
References
- ASTM-G99-95a (2000), Standard Test Method for Wear Testing with a Pin-on-Disk Apparatus, ASTM International.
- Cardinal, M.F., Castro, P.A., Baxi J., Liang, H., Williams, F.J. (2009). Characterization and frictional behavior of nanostructured Ni-W-MoS2 composite coatings. Surface and Coatings Technology, 204(1-2), 85-90.
- Charles, J., Barker, L. and Kern, W. K. (1963). Aircraft rocket launcher US 3077144 A
- Hilton, M.R. and Fleischauer,P.D. (1992). Applications of Solid Lubricant Films in Spacecraft. Surface and Coating Technology, 54-55, 435-441.
- Hou, K.-H., Wang, H.-T., Sheu, H.-H. and Ger, M.-D. (2014). Preparation and wear resistance of electrodeposited Ni–W/diamond composite coatings. Applied Surface Science, 308, 372–379.
- Huang, Z.-j. and Xiong D.-s. (2008). MoS2 coated with Al2O3 for Ni-MoS2/Al2O3 composite coatings by pulse electrodeposition. Surface and Coatings Technology, 202(14), 3208-3214.
- Saraloglu Guler, E., İ. Karakaya, and E. Konca (2013). Effect of Electrodeposition Parameters on the Current Density of Hydrogen Evolution Reaction in Ni and Ni-MoS2 Composite Coatings. Int. J. Electrochem. Sci., 8, 5496 - 5505.
- Siopis, M.J. and Cowan, R.S. (2014). Electromagnetic Launch Technology (EML). International Symposium on Electromagnetic Launch Technology, 7-11 July, San Diego, 865.