Thermal characteristics of the thermal protection material of the rocket motor case at temperatures up to 1000 oС

An experimental determination of the temperature dependences of the specific heat capacity and the thermal conductivity coefficient of the multifunctional coating MFP-92 at temperatures up to 1000 °C has been carried out. At temperatures up to 450 °C, an IT-c-400 device was used to determine the spe...

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Autores principales: Геннадий Александрович Фролов, Юрий Игоревич Евдокименко, Вячеслав Михайлович Кисель, Ирина Александровна Гусарова
Formato: article
Lenguaje:EN
RU
UK
Publicado: National Aerospace University «Kharkiv Aviation Institute» 2021
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Acceso en línea:https://doaj.org/article/0518fdc9900d4bae92fb02912fa101c0
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