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The internal ballistic analysis of a solid rocket motor mainly relies on an accurate computation of the transient burning surface geometry of the propellant during combustion phase. A reliable and an efficient burnback analysis is crucial in order to predict the ballistic performance of a solid rocket motor in early design processes.

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This page is a summary of: Internal Ballistic Modeling of a Solid Rocket Motor by Analytical Burnback Analysis, Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34065.
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