Results of studies into the properties of carbon fiber-reinforced plastics based on various polymer binders, viewed as candidates for manufacturing structures for space hardware

Автор: Akkuratov Igor Leonidovich, Alyamovskiy Andrey Ivanovich, Vinogradov Aleksey Sergeevich, Gerasimova Tatyana Ivanovna, Zemtsova Elena Vladimirovna, Kirillov Stanislav Valeryevich, Kopyl Nikolay Ivanovich, Magzhanov Rais Mukhtyasibovich, Senkovskiy Alexander Nikolayevich, Sokolova Svetlana Pavlovna, Shcherbakov Eduard Viktorovich

Журнал: Космическая техника и технологии @ktt-energia

Рубрика: Проектирование, конструкция и производство летательных аппаратов

Статья в выпуске: 1 (20), 2018 года.

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Selected for manufacturing structures of space hardware that have to bear high loads (primary structure of the front heat shield, aerodynamic shell, propulsion section body and pressurized habitable compartment) are composite materials - carbon fib er-reinforced plastics that have high specific strength and stiffness as compared with traditional structural materials. This article provides results of experimental studies on carbon plastics based on various carbon filler and polymer binders: PSB250/A, PSB250/B, PSB250/V, 22500/NIKAM-RS, KMKU-4m.175, KMU-4E, KMKU3.150.E01. The studies resulted in determining the following properties: mechanical, thermal, optical, electrical, off-gassing level in vacuum, material samples leakage using helium/air mixture, safe use parameters, including toxicology and fire safety and microbiological resistance. These properties are required for the design analysis of the above structures.

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Carbon fiber-reinforced plastic, pressurized habitable compartment, composite materials, binders, carbon fiber-reinforced plastics

Короткий адрес: https://sciup.org/143166660

IDR: 143166660

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