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

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX08CD53P
Agency Tracking Number: 070010
Amount: $100,000.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: T9.01
Solicitation Number: N/A
Solicitation Year: 2007
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-01-25
Award End Date (Contract End Date): 2009-01-23
Small Business Information
P.O. Box 186, Winona, MS, 38967-9513
DUNS: 127890197
HUBZone Owned: Y
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Jagdish Singh
 Principal Investigator
 () -
Business Contact
 William Martin
Title: Business Official
Phone: (662) 574-6688
Research Institution
 Mississippi State University
 Not Available
 205 Research Blvd.
Starkville, MS, 39759
 (662) 325-7375
 Domestic nonprofit research organization
The purity of hydrogen fuel is important in engine testing at SSC. The hydrogen may become contaminated with nitrogen, argon, or oxygen. The hydrogen from the fuel tanks 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) 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 will provide necessary information to build an improved prototype in Phase II, with better sensitivity and ease of implementation at NASA/SSC. In Phase II, a prototype LIBS system will be developed to measure impurities in H2 fuel at different places in the H2 feed line. This 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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