Design and Manufacturing Process for a Ballistic Missile

Sebastian Marian Zaharia; Rareş Ioan Ştefăneanu

doi:10.1515/bsaft-2016-0049

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Design and Manufacturing Process for a Ballistic Missile

Scientific Bulletin

Volume 21 (2016): Issue 2 (December 2016)

By: Sebastian Marian Zaharia and Rareş Ioan Ştefăneanu

Open Access

|Feb 2017

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.

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DOI: https://doi.org/10.1515/bsaft-2016-0049 | Journal eISSN: 3100-5098 | Journal ISSN: 3100-508X

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Language: English

Page range: 140 - 146

Published on: Feb 7, 2017

Published by: Nicolae Balcescu Land Forces Academy

In partnership with: Paradigm Publishing Services

Publication frequency: 2 issues per year

Keywords:

Design,

ballistic missile,

propulsion system,

manufacturing technologies

Related subjects:

Engineering,

Introductions and overviews,

Engineering, other,

Law,

Law, other,

Business and economics,

Business management,

Management, organization, corporate governance,

Social sciences,

Political science,

Military policy

© 2017 Sebastian Marian Zaharia, Rareş Ioan Ştefăneanu, published by Nicolae Balcescu Land Forces Academy
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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