arXivDaily arXiv每日学术速递 周一至周五更新
arXiv 1101.5682astro-ph.IM
收藏

毫米波空间Radio Telescope天线面形测量

Measurements of Antenna Surface for Millimeter-Wave Space Radio Telescope

Kazuhisa Kamegai, Masato Tsuboi, Akihiro Doi, Eiichi Sato

摘要:

在建造空间射电望远镜时,天线表面必须使用低噪声系数和高机械强度的材料。我们提出了两个候选人的天线表面材料的反射性能的测量结果,用于在一个新的毫米波天文卫星,ASTRO-G安装在射电望远镜。为了估计卫星预计轨道中热环境波动造成的退化量,对两种备选材料,即铜箔碳纤维增强塑料和涂铝碳纤维增强塑料进行了热循环试验。在热循环测试期间的某些点,通过使用41-45 GHz频带的辐射计精确测量表面的反射损耗。在这两种候选物中,在热循环测试后在表面上出现裂纹,其中裂纹的数量密度随着热循环的进行而增加。反射损耗也随裂纹数密度的增加而增加。然而,铜箔表面的损耗在等效寿命结束时满足ASTRO-G的要求,而铝涂层表面的损耗甚至在循环结束之前就超过了要求中的最大值。

英文摘要:

In the construction of a space radio telescope, it is essential to use materials with a low noise factor and high mechanical robustness for the antenna surface. We present the results of measurements of the reflection performance of two candidates for antenna surface materials for use in a radio telescope installed in a new millimeter-wave astronomical satellite, ASTRO-G. To estimate the amount of degradation caused by fluctuations in the thermal environment in the projected orbit of the satellite, a thermal cycle test was carried out for two candidates, namely, copper foil carbon fiber reinforced plastic (CFRP) and aluminum-coated CFRP. At certain points during the thermal cycle test, the reflection loss of the surfaces was measured precisely by using a radiometer in the 41-45 GHz band. In both candidates, cracks appeared on the surface after the thermal cycle test, where the number density of the cracks increased as the thermal cycle progressed. The reflection loss also increased in proportion to the number density of the cracks. Nevertheless, the loss of the copper foil surface met the requirements of ASTRO-G at the end of the equivalent life, whereas that of the aluminum-coated surface exceeded the maximal value in the requirement even before the end of the cycle.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

↑