Thermoplastic polymers are a compelling class of materials
for
emerging space exploration applications due to their wide range of
mechanical properties and compatibility with a variety of processing
methods, including additive manufacturing. However, despite these
benefits, the use of thermoplastic polymers in a set of critical space
applications is limited by their low electrical conductivity, which
makes them susceptible to static charging and limits their ability
to be used as active and passive components in electronic devices,
including materials for static charge dissipation, resistive heaters,
and electrodynamic dust shielding devices. Herein, we explore the
microstructural evolution of electrically conductive, surface-localized
nanocomposites (SLNCs) of chemically modified reduced graphene oxide
and a set of thermoplastic polymers as a function of critical thermal
properties of the substrate (melting temperature for semi-crystalline
materials or glass transition temperature for amorphous materials).
Selected offsets from critical substrate temperatures were used to
produce SLNCs with conductivities between 0.6–3 S/cm and surface
structures, which ranged from particle-rich, porous surfaces to polymer-rich,
non-porous surfaces. We then demonstrate the physical durability of
these electrically conductive SLNCs to expected stress conditions
for flexible conductive materials in lunar applications including
tension, flexion, and abrasion with lunar simulant. Small changes
in resistance (R/R
0 <
2) were measured under uniaxial tension up to 20% strain in high density
polyethylene and up to 500 abrasion cycles in polysulfone, demonstrating
the applicability of these materials as active and passive flexible
conductors in exterior lunar applications. The tough, electrically
conductive SLNCs developed here could greatly expand the use of polymeric
materials in space applications, including lunar exploration, micro-
and nano-satellites, and other orbital structures.