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Microgravity Propellant Gauging Using Modal Analysis

Completed Technology Project
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Project Description

Microgravity Propellant Gauging Using Modal Analysis
Low gravity propellant mass gauging is identified in NASA’s Exploratory Systems Architecture Study as a primary research challenge. The future of manned spaceflight beyond LEO relies in part on the development of accurate and robust methods of mass gauging in both settled and unsettled propellant states. We propose to utilize parabolic flights to test a novel technique for measuring the mass of liquid contained in a model propellant tank. This work continues under T0147, T0160, and T0191.
June 2015 article after second parabolic flight week: Students go weightless for research" More »

Anticipated Benefits

Primary U.S. Work Locations and Key Partners

Technology Transitions

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