Dynamic simulation analysis and optimization of firing rate of rocket launchers on wheeled vehicles

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F21%3A00557441" target="_blank" >RIV/60162694:G43__/21:00557441 - isvavai.cz</a>

Výsledek na webu

<a href="http://aimt.unob.cz/index.php/aimt/article/view/1459" target="_blank" >http://aimt.unob.cz/index.php/aimt/article/view/1459</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.3849/aimt.01459" target="_blank" >10.3849/aimt.01459</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Dynamic simulation analysis and optimization of firing rate of rocket launchers on wheeled vehicles

Popis výsledku v původním jazyce

The paper presents a method of determining the dynamic parameters of multiple-rocket-launcher system mounted on the wheeled vehicle based on Newton’s law of motion. The dynamic simulation was conducted and then the results were compared with the corresponding experimental data to verify the reliability of the model. The model was applied in calculation and tested out on multiple-rocket-launcher system BМ-21 (of Russia). The theoretical model calculation results are relatively consistent with the measured experimental data. The dependence of the launcher oscillation on the rate of fire was investigated, which determined the optimal rate of fire for each launcher. These results are used to evaluate the firing stability of the launcher when firing individual shots and firing bursts. This is an important theoretical basis which can be a reference for designers in the design process of improvement, manufacture, exploitation and use of a launcher mounted on the wheeled vehicle.

Název v anglickém jazyce

Dynamic simulation analysis and optimization of firing rate of rocket launchers on wheeled vehicles

Popis výsledku anglicky

The paper presents a method of determining the dynamic parameters of multiple-rocket-launcher system mounted on the wheeled vehicle based on Newton’s law of motion. The dynamic simulation was conducted and then the results were compared with the corresponding experimental data to verify the reliability of the model. The model was applied in calculation and tested out on multiple-rocket-launcher system BМ-21 (of Russia). The theoretical model calculation results are relatively consistent with the measured experimental data. The dependence of the launcher oscillation on the rate of fire was investigated, which determined the optimal rate of fire for each launcher. These results are used to evaluate the firing stability of the launcher when firing individual shots and firing bursts. This is an important theoretical basis which can be a reference for designers in the design process of improvement, manufacture, exploitation and use of a launcher mounted on the wheeled vehicle.

Druh

J_SC - Článek v periodiku v databázi SCOPUS

CEP obor

—

OECD FORD obor

20302 - Applied mechanics

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2021

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

Advances in Military Technology

ISSN

1802-2308

e-ISSN

2533-4123

Svazek periodika

16

Číslo periodika v rámci svazku

1

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

17

Strana od-do

159-175

Kód UT WoS článku

—

EID výsledku v databázi Scopus

2-s2.0-85112291013