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The methodology followed and the results generated to define the flight aeroheating and aerodynamic environments for NASA's successful LOFTID flight test on an inflatable hypersonics decelerators are presented.
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This page is a summary of: Aerothermodynamic Analyses for the LOFTID Technology Demonstration Mission, Journal of Spacecraft and Rockets, September 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a36009.
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