Manufacturing, thermochemical characterization and ablative performance evaluation of carbon-phenolic ablative material with nano-Al2O3 addition

Carbon-phenolic ablative materials represent the most effective solution as thermal shield for a broad kind of space missions which require a ballistic reentry in atmosphere. These materials were successfully employed for shielding probes during the reentry from the Moon and landing on Mars. Nowaday...

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Veröffentlicht in:	Polymer degradation and stability 2019-11, Vol.169, p.108979, Article 108979
Hauptverfasser:	Paglia, L., Genova, V., Marra, F., Bracciale, M.P., Bartuli, C., Valente, T., Pulci, G.
Format:	Artikel
Sprache:	eng
Schlagworte:	Ablative materials Aluminum oxide Atmospheric entry Carbon Carbon-phenolic ablators Fillers Innovations Kinetics parameters Lunar landing Lunar probes Mars Mars landing Mars missions Mars probes Mars satellites Moon Nano-alumina particles Organic chemistry Oxyacetylene Oxyacetylene flame test Performance evaluation Reentry shielding Space missions Thermogravimetric analysis Thermogravimetry
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