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Evaluation of Digital Micromirror Devices for use in space-based Multi-Object Spectrometer application

机译:用于空基的数字微镜器件的评估   多物体光谱仪应用

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摘要

The astronomical community continues to be interested in suitableprogrammable slit masks for use in multi-object spectrometers (MOSs) on spacemissions. There have been ground-based MOS utilizing digital micromirrordevices (DMDs) and they have proven to be highly accurate and reliableinstruments. This paper summarizes the results of a continuing study toinvestigate the performance of DMDs under conditions associated with spacedeployment. This includes the response of DMDs to radiation, to the vibrationand mechanical shock loads associated with launch, and the operability of DMDunder cryogenic temperatures. The optical contrast ratio and a study of thelong-term reflectance of a bare device have also been investigated. The resultsof the radiation testing demonstrate that DMDs in orbit would experiencenegligible heavy-ion induced single event upset (SEU) rate burden, we predictSEU rate of 5.6 micromirrors per 24 hours. Vibration and mechanical shocktesting was performed according to the NASA General Environmental VerificationStandard (GEVS), no mirrors failed in the devices tested. The results of lowtemperature testing suggest that DMDs are not affected by the thermal load andoperate smoothly at temperatures at least as low as 78 K. The reflectivity of abare DMD did not measurably change even after being exposed to ambientconditions over a period of 13 months. The measured contrast ratio (on state vsoff state of the DMD micromirrors) was greater than 6000/:1 when illuminatedwith an f/4 optical beam. Overall, DMDs are extremely robust and promise toprovide a reliable alternative to micro shutter arrays (MSA) to be used inspace as remotely programmable slit masks for MOS design.
机译:天文学界继续对适用于太空飞行多目标光谱仪(MOS)的可编程狭缝掩模感兴趣。已经有利用数字微镜器件(DMD)的地基MOS,它们已被证明是高度准确和可靠的仪器。本文总结了一项持续研究的结果,以调查与空间部署相关的条件下DMD的性能。这包括DMD对辐射的响应,对与发射相关的振动和机械冲击载荷的响应,以及DMD在低温下的可操作性。还研究了光学对比度和裸设备的长期反射率的研究。辐射测试的结果表明,轨道上的DMD会经历微不足道的重离子诱导的单事件翻转(SEU)速率负担,我们预测每24小时5.6微镜的SEU速率。根据NASA通用环境验证标准(GEVS)进行了振动和机械冲击测试,在所测试的设备中没有镜子发生故障。低温测试的结果表明,DMD不受热负荷的影响,并且至少在78 K的温度下即可平稳运行。即使暴露于环境中13个月后,绝对DMD的反射率也无法测量。当用f / 4光束照射时,测得的对比度(DMD微镜的开启状态与关闭状态)大于6000 /:1。总体而言,DMD极其坚固,有望提供一种可靠的替代微快门阵列(MSA),可在太空中用作MOS设计的远程可编程缝隙掩模。

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