Muscari J A, Westcott P
Appl Opt. 1975 Dec 1;14(12):2883-91. doi: 10.1364/AO.14.002883.
Final results from a part of the T027 experiment that was performed on the first Skylab mission are presented. The sample array system containing 248 optical surfaces and exposed outside the orbital workshop did not collect any significant contaminants. Unfortunate performance compromises and the relative cleanliness of the assembly on the antisolar side placed the amount of available surface contaminants at or below the limiting sensitivity of the ground measuring instruments. However, significant contamination was seen near the extravehicular hatch quadrant on the solar side of the orbiting assembly, and some results from returned samples are presented. Optical windows and mirrors exposed on the Gemini 12 mission showed degradation up to 35% in the uv wavelength region and solar absorptance increases up to 1.8 times the clean values. An expression for the attenuation coefficient vs wavelength is presented. The contaminant, a silicone base material, varied in thickness from 22 nm to 88 nm. The postflight sca ttered luminance of a contaminated Gemini 12 left-hand spacecraft hatch window was used to obtain threshold stellar visibility curves as a function of scattered and incident sunlight angles.
本文展示了在首次天空实验室任务中进行的T027实验部分的最终结果。包含248个光学表面且暴露在轨道工作室外的样本阵列系统未收集到任何显著污染物。不幸的是,性能妥协以及反太阳侧组件的相对清洁度使得可用表面污染物的量处于或低于地面测量仪器的极限灵敏度。然而,在轨道组件太阳侧的舱外舱口象限附近观察到了显著污染,并展示了返回样本的一些结果。在双子星12号任务中暴露的光学窗口和镜子在紫外波长区域的退化高达35%,太阳吸收率增加至清洁值的1.8倍。给出了衰减系数与波长的表达式。污染物为硅基材料,厚度从22纳米到88纳米不等。利用受污染的双子星12号左手航天器舱口窗口的飞行后散射亮度,获得了作为散射和入射太阳光角度函数的阈值恒星可见度曲线。