Non Intrrusive, On-line, Simultaneous Multi-Species Impurity Monitor in Hydrogen

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX09CB75C
Agency Tracking Number: 070010
Amount: $600,000.00
Phase: Phase II
Program: STTR
Awards Year: 2009
Solicitation Year: 2007
Solicitation Topic Code: T9.01
Solicitation Number: N/A
Small Business Information
P.O. Box 186, Winona, MS, 38967-9513
DUNS: 127890197
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: Y
Principal Investigator
 Perry Norton
 Principal Investigator
 () -
 norton@icet.msstate.edu
Business Contact
 Bill Martin
Title: Business Official
Phone: (662) 574-6688
Email: wvmartin@cableone.net
Research Institution
 Mississippi State University
 Not Available
 PO Box 6156
Mississippi State, MS, 39759
 (662) 325-2490
 Domestic nonprofit research organization
Abstract
The purity of hydrogen fuel is important in engine testing at SSC. The hydrogen may become contaminated with nitrogen, argon, helium or oxygen. The hydrogen from the fuel tank s or feed lines is analyzed beforehand. Therefore, there is a need for a non-intrusive, on-line, near real-time monitor for H2. The analytical technique should measure various impurities (molecular and atomic) simultaneously and be easy to implement in the field. The objective of this proposed research is to develop an analytical technique based on Laser Induced Breakdown Spectroscopy (LIBS) to measure simultaneously the concentrations of nitrogen (N2), argon (Ar), Helium (He) and oxygen (O2) contaminants in hydrogen (H2) gas storage tanks and supply lines. Advanced sensors for monitoring multiple species in H2 feed-lines and storage tanks will be useful before engine testing and will increase understanding of engine performance. Phase I has provided necessary information to build a sensitive, compact, sturdy, user-friendly and fieldable prototype in Phase II, with ease of implementation at NASA/SSC. In Phase II, a prototype LIBS system will be designed and fabricated to measure impurities in H2 fuel at different places in the H2 feed line. This integrated system will be delivered to NASA/SSC at the end of Phase II.

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

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