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A thermoanalytical study of the decomposition of a double-base propellant

✍ Scribed by F. Rodante


Publisher
Elsevier Science
Year
1986
Tongue
English
Weight
428 KB
Volume
101
Category
Article
ISSN
0040-6031

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The burning rate of a hot double-base homogeneous solid propellant is modeled by the numerical solution of the conservation equations characterizing the primary flame using a global kinetic scheme. The increase of the burning rate above the solid surface is modeled by an enhancement of the heat tran