Article ID Journal Published Year Pages File Type
6973079 Journal of Loss Prevention in the Process Industries 2016 9 Pages PDF
Abstract
A small-scale experimental apparatus is designed to study the cook-off characteristics of AP/HTPB propellant. Then a cook-off model is established according to the apparatus, and compared with the experimental results. The theoretical calculation results are in good agreement with the experimental data. On this basis, the numerical predictions of cook-off properties of a solid rocket motor are performed at different heat fluxes.
Related Topics
Physical Sciences and Engineering Chemical Engineering Chemical Health and Safety
Authors
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