Reduced Gravity Experiments to Measure Cryogenic Two-Phase Heat Transfer Coefficients for Future In-Space Transfer Systems
PI: Issam Mudawar, Purdue University, Jason Hartwig (Co-I), NASA/Glenn Research Center
PI: Issam Mudawar, Purdue University, Jason Hartwig (Co-I), NASA/Glenn Research Center
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Highly accurate flow boiling models are required to predict a spacecraft’s propellant consumption and determine the maximum allowable heating rates of the fluid. Currently, no cryogenic flow boiling data exists in the microgravity steady state.
The cryogenic steady state flow boiling data collected will be used to develop new heat transfer coefficient correlations. The data will improve the technology’s predictive capabilities, bringing it to TRL 5.
This work is a continuation of previous flight testing under T0041.
•NASA missions like Artemis, particularly for lunar and Martian ascent and descent stages
•In-space cryogenic fuel depots
•Nuclear thermal propulsion systems
•In-space commercial transfer systems
Technology Details
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Selection DateTechFlights20 (Sep 2020)
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Program StatusActive
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Development Team
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PIIssam Mudawar
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PI Organization
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Co-IJason Hartwig
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Co-I Organization
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Sponsor