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 organization of components; flight regime type, engine configuration and aerodynamic performance of the rocket flight. In this paper has been develope...

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Bibliographic Details
Published inScientific Bulletin Vol. 21; no. 2; pp. 140 - 146
Main Authors Zaharia, Sebastian Marian, Ştefăneanu, Rareş Ioan
Format Journal Article
LanguageEnglish
Published Sibiu De Gruyter Open 01.12.2016
Nicolae Balcescu
Sciendo
Subjects
Aerodynamics
Aeronautics
ballistic missile
Ballistic missiles
Clamping
Control surfaces
Cornering
Design
Gluing
High strength
Incidence angle
Maneuvers
Manufacturing
manufacturing technologies
Missile defense
Missiles
propulsion system
Rocket components
Rocket flight
Spacecraft components
Stabilizers (fluid dynamics)
Stresses
Titanium
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ISSN1224-5178
2451-3148
DOI10.1515/bsaft-2016-0049

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Summary: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.
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
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ISSN:1224-5178
2451-3148
DOI:10.1515/bsaft-2016-0049