<abstract xmlns="http://www.w3.org/1999/xhtml"><p> This paper presents the development, testing and evaluation of a new unguided rocket equipped with a thermobaric warhead. The aim of the research was to design the ammunition to be integrated with an existing multiple launch rocket system. This condition introduced limitations of dimensions, mass and mass distribution. The experimental work consisted also in optimisation of the thermobaric composition and configuration. The resulting ammunition was tested for determination of effective range and precision. The destructive effect was evaluated by live firing against non-armoured vehicles and masonry light structures.</p></abstract>

This paper presents the development, testing and evaluation of a new unguided rocket equipped with a thermobaric warhead. The aim of the research was to design the ammunition to be integrated with an existing multiple launch rocket system. This condition introduced limitations of dimensions, mass and mass distribution. The experimental work consisted also in optimisation of the thermobaric composition and configuration. The resulting ammunition was tested for determination of effective range and precision. The destructive effect was evaluated by live firing against non-armoured vehicles and masonry light structures.

Design and Testing of an Unguided Rocket with Thermobaric Warhead for Multiple Launcher System

International conference KNOWLEDGE-BASED ORGANIZATION

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.

This paper presents the development, testing and evaluation of a new unguided rocket equipped with a thermobaric warhead. The aim of the research was to design...

Design and Testing of an Unguided Rocket with Thermobaric Warhead for Multiple Launcher System

Pubblicato online: 22 lug 2017

Pagine: 188 - 198

DOI: https://doi.org/10.1515/kbo-2017-0175

Parole chiave
thermobaric, munitions, blast, energetic materials

© 2017

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.

Design and Testing of an Unguided Rocket with Thermobaric Warhead for Multiple Launcher System

Pubblicato online: 22 lug 2017

Pagine: 188 - 198

DOI: https://doi.org/10.1515/kbo-2017-0175

Parole chiavethermobaric, munitions, blast, energetic materials

© 2017

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.

Parole chiave
thermobaric, munitions, blast, energetic materials