Atomic oxygen durability of uncoated and coated high-frequency circuit materials

被引:15
作者
Gouzman, I [1 ]
Grossman, E
Lempert, G
Noter, Y
Altshuler, Y
Lifshitz, Y
机构
[1] Soreq NRC, Space Sect, IL-81800 Yavne, Israel
[2] MBT Israel Aircraft Ind Ltd, Div Elect, IL-56000 Yehud, Israel
关键词
D O I
10.1088/0954-0083/13/3/341
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
Different materials were considered for high-frequency circuit applications requiring exposure to low Earth orbit (LEO) space environment. The potential candidates were TMM3 which is a ceramic thermoset polymer composite, and RO4003 which is a glass reinforced hydrocarbon/ceramic laminate, both manufactured by Rogers Corporation (USA). Various constituents of the space environment can affect these materials' properties. Atomic oxygen is considered the most hazardous component since it may cause degradation of these materials by etching and/or changing the chemical composition. The candidate materials were tested by exposure to different equivalent atomic oxygen (ATOX) fluences of up to 1.9 X 10(21) atoms cm(-2). The effects of the atomic oxygen exposures were studied by means of scanning electron microscopy (SEM), energy dispersive x-ray spectroscopy (EDS), atomic force microscopy (AFM) and mass loss measurements. Both materials were degraded under ATOX exposure, resulting in intensive mass loss as well as changes in surface morphology and chemistry. In order to protect these materials in the LEO environment several protective coatings were evaluated for TMM3. The protective coatings tested were SiO2, CV1 144-0 (a clear silicone coating) and SG120FD (a white silicone paint). SG120FD was found to provide the best protection against ATOX irradiation attack, while CV 1144-0 provided a sufficient, though somewhat inferior protection.
引用
收藏
页码:S505 / S516
页数:12
相关论文
共 8 条
[1]  
BANKS BA, 1995, 106855 NASA
[2]  
Brundle C.R., 1992, ENCY MAT CHARACTERIZ
[3]  
Dueber R. E., 1993, CHEM PRINCIPLES APPL
[4]   ATOMIC OXYGEN TESTING WITH THERMAL ATOM SYSTEMS - A CRITICAL-EVALUATION [J].
KOONTZ, SL ;
ALBYN, K ;
LEGER, LJ .
JOURNAL OF SPACECRAFT AND ROCKETS, 1991, 28 (03) :315-323
[5]   ATOMIC OXYGEN RESISTANT COATINGS FOR LOW-EARTH-ORBIT SPACE STRUCTURES [J].
PACKIRISAMY, S ;
SCHWAM, D ;
LITT, MH .
JOURNAL OF MATERIALS SCIENCE, 1995, 30 (02) :308-320
[6]  
REDDY MR, 1992, ESA J-EUR SPACE AGEN, V16, P193
[7]  
THORNTON JA, 1982, COATING DEPOSITION S
[8]  
TOWNSEND JA, 1996, P 19 SPAC SIM C BALT, P249