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Abstract

<jats:p>Reusable spacecraft heat shields depend on an intermediate insulation layer to buffer transient heat between an outer ablative or ceramic surface and the underlying structure. The two material classes that currently occupy this layer each fail on a different axis: ceramic fibre blankets lose mechanical integrity under repeated thermal cycling, while silica aerogels, though far better insulators, are too brittle to survive routine handling and panelization. Both were optimized along a single property axis rather than against a defined thermal operating window. Here we report a ternary bacterial cellulose (BC) aerogel, crosslinked with citric acid and reinforced with poly(vinyl alcohol) and montmorillonite clay, designed explicitly for the 25–250 ◦C band that an intermediate thermal protection layer actually occupies. Differential scanning calorimetry across a four-member compositional series shows that the crosslinked, clay-loaded formulation reaches an apparent specific heat capacity of 5.63 J/(gK) by 175 ◦C, against 3.75–3.84 J/(gK) for the uncrosslinked and singly reinforced formulations, and that its principal endothermic transition shifts downward by 70–81 ◦C to 139.2 ◦C. That shift moves the material’s largest heat sink out of a region above the operating window and into it, raising energy absorbed across 130–180 ◦C from 196.5 J/g at baseline to 369.2 J/g, a 1.88-fold gain concentrated in the band that matters. Quasi-static compression shows that the same crosslinked network replaces the reproducible brittle collapse of the uncrosslinked baseline, which loses a third of its peak stress in a single discrete event at 30 % strain in every run, with a graded three-regime Gibson–Ashby response, a 12.6-fold increase in initial modulus and a roughly tenfold increase in absorbed mechanical energy, while porosity remains above 92 % and drying shrinkage below 10 %. Matching aerogel chemistry to a defined thermal window, rather than minimizing conductivity alone, offers a low-cost, freeze-dried, bio-derived route to a more durable intermediate insulation layer. It also points toward a broader design principle for any layered thermal system asked to survive a transient rather than a steady state, where thermal inertia rather than thermal resistance governs the back-face response.</jats:p>

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