Computational analysis of rocket-assisted projectile trajectory

A computational analysis was carried out in order to study the effect of solid rocket motor operating parameters on the trajectory elements of 155mm rocket-assisted projectile. Two numericalsolutions have been programmed for this purpose. The first for the rocket motor internal ballistic calculation...

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Bibliographic Details
Main Authors: Ferfouri Abdellah, Jerković Damir D., Kari Aleksandar V., Živković Saša, Karić Mirko
Format: Article
Language:English
Published: Military Technical Institute, Belgrade 2024-01-01
Series:Scientific Technical Review
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Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2024/1820-02062402009F.pdf
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