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Nanoengineered Hybrid Gas Sensors for Spacesuit Monitoring

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC19C0641
Agency Tracking Number: 150113
Amount: $754,797.00
Phase: Phase II
Program: STTR
Solicitation Topic Code: T6
Solicitation Number: STTR_19_P2S
Timeline
Solicitation Year: 2019
Award Year: 2019
Award Start Date (Proposal Award Date): 2019-09-27
Award End Date (Contract End Date): 2021-09-26
Small Business Information
9610 Medical Center Drive, #200
Rockville, MD 20850-6356
United States
DUNS: 078386164
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Ratan Debnath
 (301) 257-6756
 rdebnath@n5sensors.com
Business Contact
 Steven Brockway
Phone: (228) 813-6264
Email: Steven.M.Brockway@nasa.gov
Research Institution
 George Mason University
 
4400 University Dr
Fairfax, VA 00000-0000
United States

 Federally Funded R&D Center (FFRDC)
Abstract

N5 Sensors partnering with George Mason University (GMU) have demonstrated ultra-small, low-power gas sensors, ideally suited for integrated space suit monitoring. A single-chip carbon dioxide (CO2), oxygen (O2), and ammonia (NH3) sensors capable of operating at high-humidity conditions, different range of oxygen in the environment and with low-power consumption was demonstrated as a proof-of-concept in phase I and subsequent improvement along with system-integration was demonstrated in phase II. This was accomplished by N5rsquo;s patented innovation in photo-enabled sensing utilizing nanotechnology-based hybrid chemiresistor architecture. This unique architecture combines the selective adsorption properties of the nanophotocatalytic functional material, with the sensitive transduction capability of sub-micron semiconductor GaN structures. N5 will have a 2-fold objective for this sequential phase 2 STTR project to support the over arching goal of technology infusion to both NASA programs and commercial markets and applications ndash; 1) Improve the overall TLR of the project, and 2) Develop additional sensing capabilities suitable for both PLSS, space flight applications and also for ground based testing and other applications.

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

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