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The Australian Space Eye: Studying the History of Galaxy Formation with a CubeSat

机译:澳大利亚空间眼:用袖章研究银河系形成史

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The Australian Space Eye is a proposed astronomical telescope based on a 6 U CubeSat platform. The Space Eye will exploit the low level of systematic errors achievable with a small space based telescope to enable high accuracy measurements of the Cosmic Infrafred Background (CIB) and low surface brightness emission around nearby galaxies. To date absolute measurements of the CIB have proven elusive; the variability of atmospheric emission and scattering at these wavelengths make ground based measurements difficult while attempts to use sounding rockets have struggled to accumulate sufficient exposure time. An dedicated orbital telescope is required for a robust measurement, and Space Eye has been designed to fill this role. The scientific payload of Space Eye is a 90 mm diameter, clear aperture, all refractive telescope for wide field imaging using a set of 6 broadband filters in the i' (700-850 nm) and z' (850-1000 nm) bands. The telescope design is optimised to minimise all sources of stray light which, when combined with the advantages of the space environment, will enable the most accurate measurements of the CIB so far. This project is also a demonstrator for several technologies with general applicability to astronomical observations from nanosatellites, in particular arcsecond level instrument pointing stability and efficient image sensor temperature control. These crucial capabilities are commonplace in larger scientific satellites but have yet to be flight proven in a CubeSat platform. For the former we have developed a two stage ADCS concept combining high precision star trackers, reaction wheels, and sensor shift image stabilisation in the science instrument focal plane. Detailed system modelling, incorporating in flight performance data for many of the components, has verified that the design can achieve sub-arcsecond level pointing stability. Wc have also designed a thermal control system and concept of operations that enables passive cooling of the ima
机译:澳大利亚空间眼是一个基于6 U CubeSat平台的建议天文望远镜。空间眼将利用一个小型空间望远镜实现的低水平的系统误差,以实现宇宙陆运背景(CIB)和附近星系周围的低表面亮度排放的高精度测量。迄今为止,CIB的绝对测量已被证明是难以捉摸的;这些波长的大气排放和散射的可变性使得基于基于地面的测量困难,同时使用探测火箭队的尝试已经努力积累足够的曝光时间。坚固的测量需要专用的轨道望远镜,空间眼睛旨在填补此作用。太空眼的科学有效载荷直径为90毫米,透明孔径,所有折射望远镜,用于I'(700-850nm)和z'(850-1000nm)频段中的一组6个宽带滤波器。望远镜设计经过优化,以最大限度地减少所有杂散光源,当与空间环境的优点相结合时,将实现到目前为止的CIB最准确的测量。该项目也是几种技术的示威者,该技术具有一般适用于来自纳米卫星的天文观测,特别是弧形级仪器指向稳定性和有效的图像传感器温度控制。这些关键的能力在较大的科学卫星中是司空见惯的,但尚未在立方体平台中被证明。对于前者,我们开发了一个两个阶段ADCS概念,将高精度星跟踪器,反应轮和传感器移位图像稳定在科学仪器焦平面中结合起来。详细的系统建模,在许多组件中包含飞行性能数据,已经验证了该设计可以实现亚弧秒的指向稳定性。 WC还设计了热控制系统和操作概念,可实现IMA的被动冷却

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