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Integrated Liquid Bismuth Propellant Feed SystemA prototype bismuth propellant feed and control system was constructed and tested. An electromagnetic pump was used in this system to provide fine control of the hydrostatic pressure, and a new type of in-line flow sensor was developed to provide an accurate, real-time measurement of the mass flow rate. High-temperature material compatibility was a driving design requirement for the pump and flow sensor, leading to the selection of macor for the main body of both components. Post-test inspections of both components revealed no cracks or leaking in either. In separate proof-of-concept experiments, the pump produced a linear pressure rise as a function of current that compared favorably with theoretical pump pressure predictions, with a pressure of 10 kPa at 30 A. Flow sensing was successfully demonstrated in a bench-top test using gallium as a substitute liquid metal. A real-time controller was successfully used to control the entire system, simultaneously monitoring all power supplies and performing data acquisition duties.
Document ID
20060047750
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Polzin, Kurt A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Markusic, Thomas E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Stanojev, Boris J.
(Madison Research Corp. Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2006
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA Paper 2006-4636
Report Number: AIAA Paper 2006-4636
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Sacramento, CA
Country: United States
Start Date: July 9, 2006
End Date: July 12, 2006
Sponsors: Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Society for Engineering Education, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS7-03001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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