Miniature Sensor Probe for O2, CO2, and H2O Monitoring in Space Suits

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX13CJ02C
Agency Tracking Number: 114042
Amount: $699,961.00
Phase: Phase II
Program: SBIR
Awards Year: 2013
Solicitation Year: 2011
Solicitation Topic Code: X4.02
Solicitation Number: N/A
Small Business Information
2520 West 237th Street, Torrance, CA, 90505-5217
DUNS: 033449757
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Jesus Delgado Alonso
 Principal Investigator
 (424) 263-6321
Business Contact
 Reuben Sandler
Title: Chief Executive Officer
Phone: (424) 263-6305
Research Institution
Advanced space suits require lightweight, low-power, durable sensors for monitoring critical life support materials. No current compact sensors have the tolerance for liquid water that is specifically required for next-generation portable life support systems (PLSS). Intelligent Optical Systems (IOS) is developing a luminescence-based optical sensor probe to monitor carbon dioxide, oxygen, and humidity. Our monitor will incorporate robust CO2, O2, and H2O partial pressure sensors interrogated by a compact, low-power optoelectronic unit. The sensors will not only tolerate liquid water but will actually operate while wet, and can be remotely connected to electronic circuitry by an optical fiber cable immune to electromagnetic interference. For space systems, using these miniature sensor elements with remote optoelectronics provides unmatched design flexibility for measurements in highly constrained volume systems such as PLSS. Our flow-through monitor design includes an optical sensor we have already developed for PLSS humidity monitoring, and an optical oxygen sensor with similar IOS technology. In Phase I of this project IOS demonstrated a CO2 sensor capable of operating while wet, and a miniature prototype PPCO2-H2O-O2 sensor probe was fabricated and tested under relevant environmental conditions. In Phase II, in collaboration with Hamilton Sundstrand (Hamilton), we will design and produce prototypes for space qualification, and will conduct extensive testing under simulated space conditions, culminating in validation in NASA systems, bringing the monitor to TRL 6-7. Engineers from IOS and Hamilton will design the new sensor system to be compatible with electronics developed and fabricated for space operation by Hamilton (in particular, the common modular data bus interface unit). This approach will minimize the power requirements and size of the monitoring device, and will tremendously facilitate the infusion of the technology into the PLSS.

* Information listed above is at the time of submission. *

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