A Fast-Response Atmospheric Turbulence (FRAT) Probe with Gas-Sampling Ducts

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX09CD54P
Agency Tracking Number: 084690
Amount: $99,637.00
Phase: Phase I
Program: SBIR
Awards Year: 2009
Solicitation Year: 2008
Solicitation Topic Code: S1.08
Solicitation Number: N/A
Small Business Information
AEROPROBE
1700 Kraft Drive, Suite 2350, Blacksburg, VA, 24060-6150
DUNS: 877634105
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Demetri Telionis
 Principal Investigator
 (540) 951-3858
 demetri.telionis@aeroprobe.com
Business Contact
 Demetri Telionis
Title: Business Official
Phone: (540) 951-3858
Email: demetri.telionis@aeroprobe.com
Research Institution
N/A
Abstract
The objective of this proposal is to design, construct and test a high-frequency-response air-data probe, the Fast Response Atmospheric Turbulence probe (FRAT probe) that will be able to operate in harsh and humid atmospheric environments. Both requirements, high-frequency response and resistance to water spray can be accommodated by mounting the pressure sensors flush with the probe surface. We will also conduct research on how gas-ingesting ducts can be incorporated in the design without interference with the measuring capabilities of the probe, and we will provide for the incorporation of Anasphere's CO2 sensor. In the first phase of this effort, we will also explore the market for sensors to measure humidity and other physical quantities recommended by NASA and NOAA that can be incorporated in the base of the air-data probe. Accelerometers, magnetometers, GPS, a computer and other electronic equipment will be included to estimate the rigid-body motion of the platform carrying the probe, and then calculate velocity components with respect to an inertial frame. The final product will be the preliminary design of a stand-alone piece of instrumentation, available for mounting on a platform to measure atmospheric turbulence and the fluxes of different species and thermodynamic quantities.

* information listed above is at the time of submission.

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