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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| Autori principali: | , , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
Military Technical Institute, Belgrade
2018-01-01
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| Serie: | Scientific Technical Review |
| Soggetti: | |
| Accesso online: | https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2018/1820-02061802048T.pdf |
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