NASA/TM-210129, Martin, J.J. and Holt, J.B., Magnetically Actuated Propellant Orientation Experiment, Controlling Fluid Motion With Magnetic Fields in a Low-Gravity Environment (MSFC Center Directors Discretionary Fund Final Report, Project No. 9318), George C. Marshall Space Flight Center Marshall Space Flight Center, Alabama 35812, National Aeronautics and Space Administration Washington, DC 205460001, Prepared by Propulsion Research Center, Space Transportation Directorate, March 2000, pp. 136, Format(s): PDF 26810k |
This report details the results of a series of fluid motion experiments to investigate the use of magnets to orient fluids in a low-gravity environment. The fluid of interest for this project was liquid oxygen (LO 2) since it exhibits a paramagnetic behavior (is attracted to magnetic fields). However, due to safety and handling concerns, a water-based ferromagnetic mixture (produced by Ferrofluidics Corporation) was selected to simplify procedures. Three ferromagnetic fluid mixture strengths and a nonmagnetic water baseline were tested using three different initial fluid positions with respect to the magnet. Experiment accelerometer data were used with a modified computational fluid dynamics code termed CFX-4 (by AEA Technologies) to predict fluid motion. These predictions compared favorably with experiment video data, verifying the code's ability to predict fluid motion with and without magnetic influences. Additional predictions were generated for LO2 with the same test conditions and geometries used in the testing. Test hardware consisted of a cylindrical Plexiglas tank (6-in. bore with 10-in. length), a 6,000-G rare Earth magnet (10-in. ring), three-axis accelerometer package, and a video recorder system. All tests were conducted aboard the NASA Reduced-Gravity Workshop, a KC-135A aircraft.
| Keywords: | propellant orientation, propellant resettling, propellant transfer, propellant acquisition, magnetic control, magnetism, paramagnetic, ferromagnetic, liquid oxygen, cryogenics, low gravity, and reduced gravity |
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| Subjects: | Astronautics: Launch Vehicles And Launch Operations: Launch Vehicles |
| ID Code: | 529 |
| Deposited On: | 30 July 2002 |