What is it about?
This paper introduces a simple procedure for using pressure and thrust measurements to estimate the time-history of enlargement of the nozzle throat during firing in a typical hybrid rocket configuration.
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This page is a summary of: Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets, Journal of Propulsion and Power, November 2017, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b36390.
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