Study on performances of colorless and transparent shape memory polyimide film in space thermal cycling, atomic oxygen and ultraviolet irradiation environments

被引:47
作者
Gao, Hui [1 ]
Lan, Xin [1 ]
Liu, Liwu [2 ]
Xiao, Xinli [1 ]
Liu, Yanju [2 ]
Leng, Jinsong [1 ]
机构
[1] Harbin Inst Technol, Ctr Composite Mat & Struct, 2 Yikuang St, Harbin 150080, Heilongjiang, Peoples R China
[2] Harbin Inst Technol, Dept Astronaut Sci & Mech, 92 West Dazhi St, Harbin 150001, Heilongjiang, Peoples R China
基金
中国国家自然科学基金;
关键词
shape memory polymers; colorless and transparent shape memory polyimide films; thermal cycling; atomic oxygen; ultraviolet irradiation; MECHANICAL-PROPERTIES; POLYMERS; RADIATION; ELECTRON;
D O I
10.1088/1361-665X/aa7bd7
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Shape memory polymers with high glass transition temperature (HSMPs) and HSMP-based deployable structures and devices, which can bear harsh operation conditions for durable applications, have attracted more and more interest in recent years. In this article, colorless and transparent shape memory polyimide (SMCTPI) films were subjected to simulated vacuum thermal cycling, atomic oxygen (AO) and ultraviolet (UV) irradiation environments up to 600 h, 556 h and 600 h for accelerated irradiation. The glass transition temperature (TgW) determined by differential scanning calorimetry (DSC) and dynamic mechanical analysis (DMA) had no obvious changes after being irradiated by varying amounts of thermal cycling, AO and UV irradiation dose. After being irradiated by 50 thermal cycles, 10 x 10(21) atoms cm(-2) AO irradiation and 3000 ESH UV irradiation, shape recovery behaviors of SMCTPI films also had no obvious damage even if they experienced 30 shape memory cycles, while the surface morphologies and optical properties were seriously destroyed by AO irradiation, as compared with thermal cycling and UV irradiation. The tensile strength could separately maintain 122 MPa, 120 MPa and 70 MPa after 50 thermal cycles, 10 x 10(21) atoms cm(-2) AO irradiation and 3000 ESH UV irradiation, which shows great potential for use in aerospace structures and devices.
引用
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页数:13
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