An Instrument to Measure Aircraft Sulfate Particle Emissions

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX12CA70C
Agency Tracking Number: 105179
Amount: $749,997.00
Phase: Phase II
Program: SBIR
Awards Year: 2012
Solitcitation Year: 2010
Solitcitation Topic Code: A2.02
Solitcitation Number: N/A
Small Business Information
Aerodyne Research, Inc.
45 Manning Road, Billerica, MA, 01821-3976
Duns: 030817290
Hubzone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Jay Peck
 Principal Investigator
 (978) 932-0277
 jpeck@aerodyne.com
Business Contact
 George Wittreich
Title: Business Official
Phone: (978) 932-0215
Email: gnw@aerodyne.com
Research Institution
 Stub
Abstract
Aerodyne is developing a sulfate detection instrument, based on the Tunable Infrared Laser Differential Absorption Spectrophotometer (TILDAS) technology and therefore termed the "TILDAS-sulfate" instrument, for measurement of the size-resolved sulfate PM emissions of aircraft engine combustion. Over the past 10 years and through a series of NASA led efforts, the Aerodyne Research Inc emissions team has made a series of contributions to on-going NASA programs to characterize aircraft engine emissions. Despite progress, significant knowledge gaps exist?especially for combustion emissions of alternatives to petroleum jet fuel. During this SBIR effort, we tested instrument performance in the absence of interferences, in the presence of>20-fold excess sulfur dioxide interference, in the presence of a combustion gases containing nitrogen oxide and hydrocarbons as potential interferences, and for particles ranging in size from 100 to 300 nm. Instrument sensitivity was shown to be at least 600 ng per meter cubed (on a 1-sec cycle). In Phase II, we plan to: upgrade the instrument and incorporate improvements to Aerodyne's TILDAS technology to improve the detection limit to as low as 60 ng per meter cubed?on a 1-sec data acquisition cycle; test the upgraded instrument in the laboratory; demonstrate the instrument in the field for characterization of aircraft engine particle emissions.

* information listed above is at the time of submission.

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