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A sparse regression Legendre interval analysis approach based on the incremental finite element method is formulated to predict the life interval for aging solid-propellant rocket motor with boundary known uncertain chemical parameters.
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This page is a summary of: Life Interval Prediction for Aging Solid-Propellant Rocket Motors with Uncertain Chemical Parameters, Journal of Spacecraft and Rockets, March 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35101.
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