Review
Version 1
This version is not peer-reviewed
Polymer Nanocomposite Ablatives - Part Iii
Version 1
: Received: 12 August 2024 / Approved: 12 August 2024 / Online: 12 August 2024 (23:54:38 CEST)
How to cite: Koo, J. H.; Wagner, K.; Pilato, L. A.; Wu, H. Polymer Nanocomposite Ablatives - Part Iii. Preprints 2024, 2024080841. https://doi.org/10.20944/preprints202408.0841.v1 Koo, J. H.; Wagner, K.; Pilato, L. A.; Wu, H. Polymer Nanocomposite Ablatives - Part Iii. Preprints 2024, 2024080841. https://doi.org/10.20944/preprints202408.0841.v1
Abstract
Previous reviews by the authors [1, 2] indicate the continuing development and improvement of thermal protective systems through the introduction of polymer nanocomposites into polymer matrix composites. These materials perform as thermal protective systems for a variety of aerospace applications, such as thermal protection systems (TPS), solid rocket motors (SRM) nozzles, internal insulation of SRM, leading edges of hypersonic vehicles, and missile launch structures. A summary of the most recent, global technical research is presented. Polymeric resin systems continue to emphasize phenolic resins and other materials. New high-temperature organic resins based on phthalonitrile (PN), and polysiloxane are described and extend the increased temperature range of resin matrix systems.
Keywords
ablatives; polymer nanocomposites; nanoparticles; thermal protection systems; hypersonic vehicles, aerogels; phthalonitrile; polysiloxane; infrastructures; ballistics
Subject
Chemistry and Materials Science, Materials Science and Technology
Copyright: This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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