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We optimize the microstructure of HMX-Aluminum multi-component solid propellants so as to maximize the rate of burn, hence the performance of the propellant.
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This page is a summary of: Topology Optimization of Solid Rocket Fuel, AIAA Journal, April 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057807.
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