A numerical method for solid propellant grain design

In this study, a grain burnback analysis for an Anchor solid propellant grain geometry for a rocket motor was done. The design process involves parametric modeling of the geometry in using PTC Creo software through dynamic variables that define the complex configuration. Grain burnback is achieved b...

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Bibliographic Details
Main Authors: Tanaskovski Bojan, Nešić Jovica, Jelisavac Ljiljana, Bogdanov Jovica
Format: Article
Language:English
Published: Military Technical Institute, Belgrade 2018-01-01
Series:Scientific Technical Review
Subjects:
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2018/1820-02061802048T.pdf