Multi-Use Non-Intrusive Flow Characterization System (FCS)

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$600,000.00
Award Year:
2005
Program:
SBIR
Phase:
Phase II
Contract:
NNS05AA06C
Award Id:
67325
Agency Tracking Number:
034873
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
1212 Fourier Drive, Madison, WI, 53717
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
196894869
Principal Investigator:
Daniel Gramer
(608) 827-5000
gramerd@orbitec.com
Business Contact:
Lori Koffarnus
Business Official
(608) 827-5000
koffarnusl@orbitec.com
Research Institute:
n/a
Abstract
The product of the Phase II effort will be a Multi-Use Non-Intrusive Flow Characterization System (FCS) for densified, normal boiling point, and two-phase cryogenic flows, capable of accurately measuring several fluid parameters in real-time. Cryogenic fluids are ubiquitous in the aerospace industry; however, adequate flow instrumentation to support terrestrial, in-space, and planetary operations is currently unavailable. FCS was originated to address this issue and greatly enhance the quantification, reliability, and safety of propulsion test operations, as well as reduce operational expenses. FCS will also play a significant role in initiatives for the exploration of the Moon and Mars through supporting the design, development, and operation of gravity-dependant processes. FCS handles both transient and steady state flows, and can operate in the following five modes: (1) on-line analysis of fluid mixtures; (2) mass flow rate measurement; (3) temperature measurement; (4) fluid conditioning and health monitoring; and (5) model validation for a cryogenic or non-cryogenic fluid flow. The Phase II effort will develop an FCS system that has broad application throughout NASA and the rest of the aerospace community. A fully functional FCS system will be delivered to NASA/SSC upon completion of the program for use in the E1 or other facility.

* information listed above is at the time of submission.

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