Hydrogen detection by SnO2 gas sensors
Résumé
For the Ariane vehicle system development, studies leaded to prevent fire and explosion risks mainly on account of hydrogen and oxygen on board of the launcher: the leckage detection (02, H2) was one of the studies axis. This activity concerned the detection systems of H2 and/or O2 in terms of operational needs for a launcher: measure principle, instrumentation used in industry or in Research/Development, performances and reliability. Hydrogen detection is possible with various physical or chemical technics. The choice of the method depends on the performances which are inquire for a special application: on one hand, the measurement performances (sensitivity, selectivity, stability, reproducibility, calibration needs, ...) and on the other hand, the operational parameters such as cost, dimensions, weight, power supply,... An evaluation of these detection systems (catalyst detector, thermal conductivity, electrochemical oxidation, optical interferometry, thin film detector, ...) based on Nasa data [1] showed the interest of the semi-conductor sensors: nevertheless an accurate evaluation of these sensors performance is essential to consider their possible utilization for Ariane 5. Also, a research activity, beared by the CNES (the French Space Agency: Ariane Launcher Direction) and managed by the AEROSPATIALE (Industrial Architect of Ariane 5) was leaded by Saint-Etienne Mines School. The aim was to evaluate the SnO-z semi-conductor sensors performance, i.e. their selectivity, sensibility, response linearity, response delay, drift during time,... For all these parameters, the effect of the temperature and oxygen traces was studied.
Domaines
Génie des procédés
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