The advantaged mass-specific properties of aligned nanofibers, such as aligned carbon nanotubes (A-CNTs), and their facile densification into uniformly high volume fraction (V f , commonly vol%) architectures motivates their use as dense reinforcement for aerospace composites and bulk nanostructured materials. Since tuning A-CNT array packing density is essential to improve polymer nanocomposite (PNC) properties, this work presents an experimental process-structure study to understand how the nano-, meso-, and micro-scale structure of aerospace-grade composite matrices, specifically an epoxy thermoset polymer, is affected by high levels of A-CNT confinement (i.e. inter-CNT spacings on the order of nm), and demonstrates that processing of these PNCs is achievable at relatively high CNT V f . In this report, A-CNT/aerospace-grade epoxy matrix PNCs with mm-tall densified A-CNT reinforcement are fabricated, and their process-structure-property relationships are analyzed as a function of CNT V f via scanning electron microscopy, X-ray micro-computed tomography, Raman spectroscopy, and quasi-static nanoindentation testing. These analyses provide multi-scale information to show how CNT confinement in dense arrays from 1 − 30 vol% influences polymer infiltration, wetting, structural evolution, and CNT-matrix morphology, including PNC fracture surfaces. The findings from this work provide new insight into the processability of aerospace-grade resins into densely packed A-CNT arrays to facilitate manufacturing, and they provide process-structure-property relationships to support the design of next-generation composite materials with increased A-CNT reinforcement. Nomenclature A-CNT aligned carbon nanotube CNT carbon nanotube Γ inter-CNT spacing PNC polymer nanocomposite SEM scanning electron microscopy CNT V f carbon nanotube volume fraction X-ray µCT X-ray micro-computed tomography