Solid Propellant Grain Configuration with Progressive Burning Obtained Through Additive Manufacturing

Data publikacji: 19 lip 2023

Zakres stron: 38 - 42

DOI: https://doi.org/10.2478/kbo-2023-0073

Słowa kluczowe

solid rocket motor, propellant grain, unsteady lumped internal ballistic model, additive manufacturing, FDM

© 2023 Marius-Ionuț Mărmureanu et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.