High-voltage and high-power devices are indispensable
in spacecraft
for outer space explorations, whose operations require aerospace materials
with adequate vacuum surface insulation performance. Despite persistent
attempts to fabricate such materials, current efforts are restricted
to trial-and-error methods and a universal design guideline is missing.
The present work proposes to improve the vacuum surface insulation
by tailoring the surface trap state density and energy level of the
metal oxides with varied bandgaps, using coating on a polyimide (PI)
substrate, aiming for a more systematical workflow for the insulation
material design. First-principle calculations and trap diagnostics
are employed to evaluate the material properties and reveal the interplay
between trap states and the flashover threshold, supported by dedicated
analyses of the flashover voltage, secondary electron emission (SEE)
from insulators, and surface charging behaviors. Experimental results
suggest that the coated PI (i.e., CuO@PI, SrO@PI, MgO@PI, and Al2O3@PI) can effectively increase the trap density
and alter the trap energy levels. Elevated trap density is demonstrated
to always yield lower SEE. In addition, increasing shallow trap density
accelerates surface charge dissipation, which is favorable for improving
surface insulation. CuO@PI exhibits the most remarkable increase in
shallow trap density, and accordingly, the highest flashover voltage
is 42.5% higher than that of pristine PI. This study reveals the critical
role played by surface trap states in flashover mitigation and offers
a novel strategy to optimize the surface insulation of materials.