Thesis_A Review of Erosive Burning Models for Solid Propellant.xlsx (2.85 MB)

A Review of Erosive Burning Models for Solid Propellant Rocket Motors (Spreadsheet)

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posted on 27.07.2021, 09:13 by Daniel Macêdo-Gonçalves
This spreadsheet, an integral part of the thesis "A Review of Erosive Burning Models for Solid Propellant Rocket Motors" (Guided Weapon Systems MSc, 2020/2021), presents a useful tool in modelling the erosive burning rate of composite and double-base propellants, from modifications to the theoretical model originally proposed by Paul and Mukunda (1997).

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Authoriser (e.g. PI/supervisor)

d.bray@cranfield.ac.uk