Wang Zhenzhong, Ren Xi, Zhang Yan, Yang Changxu, Han Shujun, Qi Yuexin, Liu Jingang
Engineering Research Center of Ministry of Education for Geological Carbon Storage and Low Carbon Utilization of Resources, School of Materials Science and Technology, China University of Geosciences, Beijing 100083, China.
Polymers (Basel). 2024 Jan 26;16(3):343. doi: 10.3390/polym16030343.
Colorless and transparent polyimide (CPI) films with good atomic oxygen (AO) resistance and high thermal endurance are highly required in low earth orbit (LEO) space exploration. Conventional CPI films based on fluoro-containing 4,4'-(hexafluoroisopropylidene)diphthalic anhydride (6FDA) have been widely used in space applications. However, the AO erosion yields and glass transition temperatures (T) of the 6FDA-based CPI films have to be modified in order to meet the severe serving environments. In the current work, novel CPI films based on a multi-ring fluoro-containing 9,9-bis(trifluoromethyl)xanthene-2,3,6,7-tetracarboxylicdianhydride (6FCDA) monomer were developed. In order to enhance the AO resistance of the derived CPI film, a phosphorus-containing aromatic diamine, 2,5-bis[(4-aminophenoxy)phenyl]diphenylphosphine oxide (BADPO) was used to polymerize with the dianhydride to create the organo-soluble resin. Then, two phosphorus-containing CPI films (PPI), including PPI-1 (6FDA-BADPO) and PPI-2 (6FCDA-BADPO) were prepared by thermally curing of the PPI solutions at elevated temperatures. The PPI films maintained good optical transparency with transmittance values over 80% at a wavelength of 450 nm. PPI-2 exhibited a T value of 311.0 °C by differential scanning calorimetry (DSC) measurement, which was 46.7 °C higher than that of the PPI-1 counterpart (T = 264.3 °C). In addition, the PPI-2 film showed a coefficient of linear thermal expansion (CTE) value of 41.7 × 10/K in the range of 50~250 °C, which was apparently lower than that of the PPI-1 sample (CTE = 49.2 × 10/K). Lastly, both of the two PPI films exhibited good AO resistance with the erosion yields (E) of 6.99 × 10 cm/atom for PPI-1 and 7.23 × 10 cm/atom for PPI-2 at an exposure flux of 5.0 × 10 atoms/cm. The E values of the current PPI films were obviously lower than that of the standard polyimide (PI) film based on pyromellitic dianhydride (PMDA) and 4,4'-oxydianiline (ODA) (E = 3.0 × 10 cm/atom).
在低地球轨道(LEO)空间探索中,对具有良好抗原子氧(AO)性能和高耐热性的无色透明聚酰亚胺(CPI)薄膜有很高的需求。基于含氟的4,4'-(六氟异丙基)二邻苯二甲酸酐(6FDA)的传统CPI薄膜已广泛应用于太空领域。然而,为了满足严苛的服役环境,必须对基于6FDA的CPI薄膜的AO侵蚀产率和玻璃化转变温度(T)进行改进。在当前工作中,开发了基于多环含氟的9,9-双(三氟甲基)氧杂蒽-2,3,6,7-四羧酸二酐(6FCDA)单体的新型CPI薄膜。为了提高所得CPI薄膜的抗AO性能,使用含磷芳香二胺2,5-双[(4-氨基苯氧基)苯基]二苯基氧化膦(BADPO)与二酐聚合以制备有机可溶性树脂。然后,通过在高温下热固化PPI溶液制备了两种含磷的CPI薄膜(PPI),包括PPI-1(6FDA-BADPO)和PPI-2(6FCDA-BADPO)。PPI薄膜保持了良好的光学透明度,在450nm波长处的透光率值超过80%。通过差示扫描量热法(DSC)测量,PPI-2的T值为311.0℃,比PPI-1对应物(T = 264.3℃)高46.7℃。此外,PPI-2薄膜在50~250℃范围内的线性热膨胀系数(CTE)值为41.7×10⁻⁶/K,明显低于PPI-1样品(CTE = 49.2×10⁻⁶/K)。最后,在5.0×10¹³原子/cm²的辐照通量下,两种PPI薄膜均表现出良好的抗AO性能,PPI-1的侵蚀产率(E)为6.99×10⁻²⁴cm³/原子,PPI-2为7.23×10⁻²⁴cm³/原子。当前PPI薄膜的E值明显低于基于均苯四甲酸二酐(PMDA)和4,4'-二氨基二苯醚(ODA)的标准聚酰亚胺(PI)薄膜(E = 3.0×10⁻²³cm³/原子)。