Abstract

Molybdenum disulfide is one of the most common lubricant coatings for space systems but it displays enormous susceptibility to environmental conditions making it hard to predict performance throughout the entire lifetime. The majority of mechanisms for space operate in low Earth orbit where temperatures typically reach 120 °C along with exposure to highly reactive atomic oxygen which can be detrimental to lubricant performance. In the present study, a MoS2 lubricant coating is tested using friction force microscopy under different environmental conditions including air and dry nitrogen environments with temperatures ranging from 25 °C to 120 °C. The increased temperature was found to be beneficial for friction behaviour in air up to 100 °C as ambient humidity is removed from the contact, but higher temperatures become detrimental as increased reactivity leads to oxidation. These competing effects resulted in a minimum coefficient of friction at 110 °C in the air environment. The high temperature also increases the wear of the coatings as the intrinsic shear strength decreases with thermal energy which in turn disrupts tribofilm formation leading to increased friction. The run-in duration and magnitude are both found to decrease with temperature as the energy barrier to optimal reconfiguration is reduced. Finally, contextualization of the present findings for mechanisms operating in low earth orbit is discussed.

Highlights

  • Friction and wear of space systems is a multifaceted problem facing extreme conditions rarely encountered or engineered for on Earth

  • Seven temperatures ranging from 25 ◦ C to 120 ◦ C for ambient air environments and three temperatures for inert nitrogen environments were studied

  • For the tests in air, the friction is found to decrease with respect to temperature until 110 ◦ C and begin to increase again at 120 ◦ C

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Summary

Introduction

Friction and wear of space systems is a multifaceted problem facing extreme conditions rarely encountered or engineered for on Earth. Extreme operating temperatures, radiation, and inability to perform maintenance are among the basic challenges which all contribute to the collective difficulty in providing long-lasting and predictable lubrication for space systems [1]. Lubrication for space takes three main forms: liquid (predominantly synthetic oils), grease (liquid lubricants with a thickener), or solid (materials with low interfacial shear strength and surface energy) [2]. Vacuum outgassing [4] and offer excellent thermal stability [5]. Thermal stability and durability in vacuum are two of the most prominent advantages of solid lubricant coatings and are especially favourable for the dominant space-qualified solid lubricant, molybdenum disulfide (MoS2 ).

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