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Temperature and displacement rate significantly influence the mechanical responses of HTPB-based composite solid propellants, with lower temperatures leading to higher failure stress and earlier void initiation, while higher displacement rates increase failure stress, failure strain, and tensile modulus. Novelty: ClaimNovelty.INCREMENTAL. Consensus alignment: ConsensusAlignment.NEUTRAL.

Elucidating Damage Evolution in HTPB-Based Composite Propellants under Varying Displacement Rates and Temperatures using Dual-Surface 2D-DIC

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