A Novel Flow Measurement System for Cryogenic Two-Phase Flow

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$125,000.00
Award Year:
2012
Program:
SBIR
Phase:
Phase I
Contract:
NNX12CD92P
Agency Tracking Number:
115475
Solicitation Year:
2011
Solicitation Topic Code:
X10.01
Solicitation Number:
n/a
Small Business Information
En'Urga Inc
1291-A Cumberland Avenue, West Lafayette, IN, 47906-1385
Hubzone Owned:
N
Socially and Economically Disadvantaged:
Y
Woman Owned:
N
Duns:
944533009
Principal Investigator:
Ye Mi
Principal Investigator
(765) 497-3269
yemi@enurga.com
Business Contact:
Ye Mi
Research Scientist
(765) 497-3269
yemi@enurga.com
Research Institution:
Stub




Abstract
Flow rate measurements for cryogenic propellants are required for spacecraft and space exploration systems. Such a requirement has been hampered by lack of fast and accurate instruments among existing technologies. This proposed project will develop a mass flow measurement system for non-conducting cryogenic propellant flow to meet the NASA's need. In the proposed system, an electromagnetic flowmeter for insulating fluids (EMFIF) will be able to provide real-time liquid velocity information under single- and two-phase flow conditions, and an X-ray void fraction sensor will provide phase concentration and interfacial velocity information. The X-ray sensor will also be able to detect bubble existence in cryogenic propellant flow. The whole proposed system will be a useful instrument to measure propellant flowrate in rocket engine feed lines.During the Phase I project, a test model of the proposal measurement technique will be designed and built. The performance of the proposed flowmeter will be studied in an experimental cross-calibration. If the Phase I study shows that it is feasible to employ the flowmeter for single/two-phase flow, the Phase II development towards engineering design and verification of the system will be carried out.

* information listed above is at the time of submission.

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