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Proceedings Paper

Integrated multi-channel nano-engineered optical hydrogen and temperature sensor detection systems for launch vehicles
Author(s): M. Z. Alam; J. Moreno; J. S. Aitchison; M. Mojahedi; A. A. Kazemi
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Paper Abstract

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. This 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. Like 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.

Paper Details

Date Published: 26 August 2008
PDF: 7 pages
Proc. SPIE 7095, Nanophotonics and Macrophotonics for Space Environments II, 70950O (26 August 2008); doi: 10.1117/12.807651
Show Author Affiliations
M. Z. Alam, Univ. of Toronto (Canada)
J. Moreno, Univ. of Toronto (Canada)
J. S. Aitchison, Univ. of Toronto (Canada)
M. Mojahedi, Univ. of Toronto (Canada)
A. A. Kazemi, The Boeing Co. (United States)

Published in SPIE Proceedings Vol. 7095:
Nanophotonics and Macrophotonics for Space Environments II
Edward W. Taylor; David A. Cardimona, Editor(s)

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