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Integrated multi-channel nano-engineered optical hydrogen and temperature sensor detection systems for launch vehicles

机译:用于运载火箭的集成多通道纳米工程光学氢和温度传感器检测系统

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Launch vehicles and other satellite users need launch services that are highly reliable, less complex, easier to test, and cost effective. Being a very small molecule, hydrogen is prone to leakage through seals and micro-cracks. Hydrogen detection in space application is very challenging; public acceptance of hydrogen fuel would require the integration of a reliable hydrogen safety sensor. For detecting leakage of cryogenic fluids in spaceport facilities, launch vehicle industry and aerospace agencies are currently relying heavily on the bulky mass spectrometers, which fill one or more equipment racks, and weigh several hundred kilograms. Therefore, there is a critical need for miniaturized sensors and instruments suitable for use in space applications.rnThis paper describes a novel multi-channel integrated nano-engineered optical sensor to detect hydrogen and monitor the temperature. The integrated optic sensor is made of multi-channel waveguide elements that measure hydrogen concentration in real Time. Our sensor is based on the use of a high index waveguide with a Ni/Pd overlay to detect hydrogen. When hydrogen is absorbed into the Ni/Pd alloy there is a change in the absorption of the material and the optical signal in the waveguide is increased. Our design uses a thin alloy (few nanometers thick) overlay which facilitates the absorption of the hydrogen and will result in a response time of approximately few seconds.rnLike other Pd/Pd-Ni based sensors the device response varies with temperature and hence the effects of temperature variations must be taken into account. One solution to this problem is simultaneous measurement of temperature in addition to hydrogen concentration at the same vicinity. Our approach here is to propose a temperature sensor that can easily be integrated on the same platform as the hydrogen sensor reported earlier by our group. One suitable choice of material system is silicon on insulator (SOI). Here, we propose a micro ring resonators (MRR) based temperature sensor designed on SOI that measures temperature by monitoring the output optical power.
机译:运载火箭和其他卫星用户需要高度可靠,复杂程度较低,易于测试且具有成本效益的运载服务。作为一个很小的分子,氢易于通过密封件和微裂纹泄漏。太空应用中的氢气检测非常具有挑战性。公众接受氢燃料将需要集成可靠的氢安全传感器。为了检测太空港设施中低温流体的泄漏,运载火箭工业和航空航天机构目前严重依赖于庞大的质谱仪,该质谱仪充满了一个或多个设备机架,重达数百公斤。因此,迫切需要适合空间应用的小型传感器和仪器。本文介绍了一种新颖的多通道集成纳米工程光学传感器,用于检测氢气和监测温度。集成的光学传感器由可实时测量氢浓度的多通道波导元件组成。我们的传感器基于使用高折射率波导和Ni / Pd覆盖层来检测氢。当氢被吸收到Ni / Pd合金中时,材料的吸收会发生变化,波导中的光信号会增加。我们的设计使用了薄合金(几纳米厚)的覆盖层,该覆盖层促进了氢的吸收并会导致大约几秒钟的响应时间。与其他基于Pd / Pd-Ni的传感器一样,该器件的响应会随温度而变化,因此影响必须考虑温度变化的影响。解决该问题的一种方法是,除了在同一附近测量氢气浓度外,还同时测量温度。我们在这里的方法是提出一种温度传感器,该温度传感器可以与我们小组先前报道的氢传感器轻松集成在同一平台上。材料系统的一种合适选择是绝缘体上硅(SOI)。在这里,我们提出了一种基于微环谐振器(MRR)的基于SOI的温度传感器,该传感器通过监视输出光功率来测量温度。

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