Process-Hardened, Multi-Analyte Sensor for Characterizing Rocket Plum Constituents Under Test Environment

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$100,000.00
Award Year:
2008
Program:
STTR
Phase:
Phase I
Contract:
NNX08CD51P
Agency Tracking Number:
070117
Solicitation Year:
2007
Solicitation Topic Code:
T9.01
Solicitation Number:
n/a
Small Business Information
Innosense, LLC
2531 West 237th Street, Suite 127, Torrance, CA, 90505-5245
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
Y
Duns:
114060861
Principal Investigator:
Shelly Mechery
Principal Investigator
(310) 530-2011
shelly.mechery-1@innosense.us
Business Contact:
Latika Datta
Chief Operational Officer
(310) 530-2011
latika.datta@innosense.us
Research Institution:
University of Tennessee
Not Available
1534 White Avenue
Knoxville, TN, 37996
(865) 974-3466
Domestic nonprofit research organization
Abstract
This STTR project aims to develop a process-hardened, simple and low cost multi-analyte sensor for detecting components of rocket engine plumes. The sensor will be constructed with materials for operating continuously at 550 OK. It will also withstand temperatures as high as 2100 OK for at least five seconds. NASA roadmaps point towards new hydrocarbon fueled engines. A non-intrusive instrument suitable for monitoring plume signature with high degree of reliability will facilitate this future development. Tasks are designed to establish the device feasibility by detecting carbon dioxide and kerosene in air over 0-1% (v/v) range in the presence of 100% moisture. The sensor array chip is capable of holding indicators for tens of analytes. A major aerospace company has expressed strong interest in the proposed technology for integrating in their test facilities. InnoSense LLC (ISL) will develop, characterize and field-test the prototype in Phase II. For assuring success of this project, ISL has assembled a technical team with a cumulative 90 person-years of experience in developing commercially viable sensor systems.

* information listed above is at the time of submission.

Agency Micro-sites

US Flag An Official Website of the United States Government