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METHOD FOR ANALYSING AND CALCULATING STRUCTURAL DEVIATION CHARACTER OF BALISTIC MISSILE

Mas Zhao

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Abstract

A method for analysing and calculating basic structural deviation charactors of a missile was proposed. For illustrating present method, a two-stagy liquid-propellant missile, as an example, was analysed. A method can rationalize the design of missile system further, therefor, can be extended to design for the carrier rocket and other kinds of missile.

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What this paper is about

A method for analysing and calculating basic structural deviation charactors of a missile was proposed. For illustrating present method, a two-stagy liquid-propellant missile, as an example, was analysed. A method can rationalize the design of missile system further, therefor, can be extended to design for the carrier rocket and other kinds of missile.

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Available abstract

A method for analysing and calculating basic structural deviation charactors of a missile was proposed. For illustrating present method, a two-stagy liquid-propellant missile, as an example, was analysed. A method can rationalize the design of missile system further, therefor, can be extended to design for the carrier rocket and other kinds of missile.

Key concepts: Missile, Rocket (weapon), Character (mathematics), Aerospace engineering, Propellant, Engineering, Structural engineering, Computer science

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