<abstract xmlns="http://www.w3.org/1999/xhtml"><p>Designing a ballistic missile flight depends on the mission and the stress to which the missile is subject. Missile’s requests are determined by: the organization of components; flight regime type, engine configuration and aerodynamic performance of the rocket flight. In this paper has been developed a ballistic missile with a smooth fuselage type, 10 control surfaces, 8 directional surfaces for cornering execution, 2 for maneuvers of execution to change the angle of incidence and 4 stabilizers direction. Through the technology of gluing and clamping of the shell and the use of titanium components, mass of ballistic missile presented a significant decrease in weight and a structure with high strength.</p></abstract>

Designing a ballistic missile flight depends on the mission and the stress to which the missile is subject. Missile’s requests are determined by: the organization of components; flight regime type, engine configuration and aerodynamic performance of the rocket flight. In this paper has been developed a ballistic missile with a smooth fuselage type, 10 control surfaces, 8 directional surfaces for cornering execution, 2 for maneuvers of execution to change the angle of incidence and 4 stabilizers direction. Through the technology of gluing and clamping of the shell and the use of titanium components, mass of ballistic missile presented a significant decrease in weight and a structure with high strength.

Design and Manufacturing Process for a Ballistic Missile

Transilvania University of Braşov, Braşov,

Nuarb Training Academy & Nuarb Aerospace, Braşov,

Scientific Bulletin

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

{"article-title":"Design and Manufacturing Process for a Ballistic Missile"}

Designing a ballistic missile flight depends on the mission and the stress to which the missile is subject. Missile’s requests are determined by: the...

Design and Manufacturing Process for a Ballistic Missile

Publicado en línea: 07 feb 2017

Páginas: 140 - 146

DOI: https://doi.org/10.1515/bsaft-2016-0049

Palabras clave
Design, ballistic missile, propulsion system, manufacturing technologies

© 2015 Sebastian Marian Zaharia et al., published by De Gruyter Open

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

Design and Manufacturing Process for a Ballistic Missile

Publicado en línea: 07 feb 2017

Páginas: 140 - 146

DOI: https://doi.org/10.1515/bsaft-2016-0049

Palabras claveDesign, ballistic missile, propulsion system, manufacturing technologies

© 2015 Sebastian Marian Zaharia et al., published by De Gruyter Open

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

Palabras clave
Design, ballistic missile, propulsion system, manufacturing technologies