En'urga Inc
- View government funding actions
- West Lafayette, IN 479061385
- Phone: 765-497-3269
- Corporate URL: www.enurga.com
- Estimated Number of Employees: 9
- Estimated Annual Receipts: $1,200,000
- Business Start Date: 1994
- Contact Person: Yudaya Sivathanu
- Contact Phone: 765-497-3269
- Contact Email: sivathan@enurga.com
- Business Structure:
- Corporate Entity (Not Tax Exempt)
- Business Type:
- Minority Owned Business
- For Profit Organization
- Manufacturer of Goods
- Subcontinent Asian (Asian-Indian) American Owned
- Industries Served: Engineering Services, Testing Laboratories, Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology), All Other Professional, Scientific, and Technical Services
- Product Areas: R&D- ECONOMIC GROWTH: MANUFACTURING TECHNOLOGY (ENGINEERING DEVELOPMENT), R&D-MANUFACTURING TECH-ENG DEV, R&D- GENERAL SCIENCE/TECHNOLOGY: PHYSICAL SCIENCES (ENGINEERING DEVELOPMENT), PHYSICAL SCIENCES (ENGINEERING), R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (ENGINEERING DEVELOPMENT), R&D-AERO & SPACE TECH-ENG DEV, R&D- OTHER RESEARCH AND DEVELOPMENT (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT), R&D-OTHER R & D-A RES/EXPL DEV
Sampling of Federal Government Funding Actions/Set Asides
In order by amount of set aside monies.
- $253,998 - Wednesday the 30th of January 2013
Federal Railroad Administration
DEPT OF TRANS/FEDERAL RAILROAD ADMIN
IGF::OT::IGF INSTALLATION OF TEMPERTURE SENSOR ON FRA'S TEST RAIL CAR - $150,000 - Wednesday the 20th of June 2012
Department Of Air Force
FA9300 AFTC PZR
SBIR I ENURGA - $125,000 - Thursday the 28th of March 2013
National Aeronautics And Space Administration
NASA SHARED SERVICES CENTER
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.
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