Passive heat management is crucial in space, especially
for extended
missions involving protection from sunlight. Thermal coatings with
desirable optical properties can drastically reduce the power consumed
by active cooling systems, thereby reserving more resources for other
critical systems onboard. Specifically, materials with wavelength-dependent
reflectance and emittance are desirable for managing incident sunlight
and self-cooling by thermal emission. This study demonstrates the
use of polymer nanofibers, specifically poly(tetrafluoroethylene)
(PTFE), for passive temperature control in space applications. This
study describes the electrospinning fabrication process to create
nanofibers and how process parameters can be varied to control the
fiber geometry. We combine poly(tetrafluoroethylene) (PTFE) and poly(ethylene
oxide) (PEO) polymers to fabricate highly reflective thermal control
materials by electrospinning. To understand the role of material and
fiber geometry, we measure spectral reflectance, absorptance, and
transmittance using spectrophotometers interfaced with integrating
spheres. We control the materials’ fiber geometry and solar
reflectance by modifying the solution properties, flow rate, rotating
collector speed, and fabrication time. With 220–1560 μm
thick electrospun nanofiber materials, we demonstrate an average solar
reflectance of 94.73–99.75%, with values approaching 99.9%
for thicker samples, which is among the highest for space applications.
Meanwhile, a thermal emittance of 81.4% was observed at 300 K for
a 3360 μm thick sample. The durability of these samples was
also tested under ultraviolet light and atomic oxygen. Compared to
the state-of-the-art materials, the electrospun
PTFE–PEO fibers present a new paradigm for passive thermal
management in space applications.