Holtzclaw K W, Fraser M E, Gelb A, Green B D
Appl Opt. 1994 Aug 1;33(22):5062-7. doi: 10.1364/AO.33.005062.
Large optical telescopes are being placed into orbit at altitudes where the residual atmosphere can interact with the spacecraft to produce optical emissions, such as the visible shuttle glow. The near-field emissions produced from these interactions will reduce the far-field detection limits of these instruments. Here we present laboratory data on the intensities and spectral distributions of the infrared emissions created in the interaction at orbital velocity of the dominant atmospheric constituent, atomic oxygen, with optical baffle coating materials used on space observatory platforms: Z306 Chemglaze paint, black anodized aluminum, and black Teflon. Data over the 1.0-5.4-µm spectral region are presented. Adsorbed contaminants dominate the spectra of the less reactive coatings. We present data on contaminant removal with oxygen fluence. We also include a simple assessment, based on these data, of the magnitude of this interaction and its effect on mission performance.
大型光学望远镜正被放置在一定高度的轨道上,在这个高度,残余大气会与航天器相互作用产生光发射,比如可见的航天飞机辉光。这些相互作用产生的近场发射会降低这些仪器的远场探测极限。在此,我们展示了关于在轨道速度下,主要大气成分原子氧与空间天文台平台上使用的光学挡板涂层材料(Z306 Chemglaze漆、黑色阳极氧化铝和黑色特氟龙)相互作用时产生的红外发射的强度和光谱分布的实验室数据。给出了1.0 - 5.4微米光谱区域的数据。吸附的污染物在反应性较低的涂层光谱中占主导。我们展示了去除污染物的氧注量数据。我们还基于这些数据对这种相互作用的量级及其对任务性能的影响进行了简单评估。