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...
Guardado en:
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
|
Materias: | |
Acceso en línea: | https://doaj.org/article/0518fdc9900d4bae92fb02912fa101c0 |
Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
Ejemplares similares
-
Thermal characteristics of the heat protection package of the engine body at programmed heating
por: Юрий Игоревич Евдокименко, et al.
Publicado: (2021) -
Remote support and upgrade of program-technical complex for aircraft engines testing
por: Вадим Владимирович Нерубасский, et al.
Publicado: (2021) -
Regulator for engine MC-500 – development, testing, certification
por: Анна Григорьевна Буряченко, et al.
Publicado: (2021) -
Development of a stand for measuring metrological characteristics of electric motors
por: Володимир Павлович Квасніков, et al.
Publicado: (2021) -
Improvement of mixing processes in the combustion chamber of thermal engines
por: Ирина Владимировна Морозова, et al.
Publicado: (2021)