Flight Hydrogen Sensor for Use in the ISS Oxygen Generation Assembly

2005-01-2870

07/11/2005

Event
International Conference On Environmental Systems
Authors Abstract
Content
This paper provides a description of the hydrogen sensor Orbital Replacement Unit (ORU) used on the Oxygen Generation Assembly (OGA), to be operated on the International Space Station (ISS). Makel Engineering, Inc. (MEI) is providing the hydrogen sensor ORU to monitor the oxygen outlet for the presence of hydrogen. The hydrogen sensor ORU is a triple redundant design where each sensor converts raw measurements to actual hydrogen partial pressure that is reported to the OGA system controller. The signal outputs are utilized for system shutdown in the event that the hydrogen concentration in the oxygen outlet line exceeds the specified shutdown limit. Improvements have been made to the Micro-Electro-Mechanical Systems (MEMS) based sensing element, screening, and calibration process to meet OGA operating requirements. Two flight hydrogen sensor ORUs have successfully completed the acceptance test phase. This paper also describes the sensor’s performance during acceptance testing, additional tests planned to extend the operational performance calibration cycle, and integration with the OGA system.
Meta TagsDetails
DOI
https://doi.org/10.4271/2005-01-2870
Pages
8
Citation
M’Sadoques, G., and Makel, D., "Flight Hydrogen Sensor for Use in the ISS Oxygen Generation Assembly," SAE Technical Paper 2005-01-2870, 2005, https://doi.org/10.4271/2005-01-2870.
Additional Details
Publisher
Published
Jul 11, 2005
Product Code
2005-01-2870
Content Type
Technical Paper
Language
English