Determining the aerodynamic parameters of a solid-propellant high-speed Aerial target
Keywords:
Aerial target, Aerodynamic parameters, Solid propellantAbstract
The Aerial target using solid propellants rocket motors (MTB01) is researched, designed and manufactured new types of cruise missiles, controlled, surface to surface, two-stage solid propellants rocket motors, carrying infrared emission clusters and radio reflectors, the target is used as a target in training firing for some types of air defense missiles. This paper presents the aerodynamic results of the Aerial target MTB01. These results are the input to the simulation program, which is used to assess the trajectory of the Aerial target based on the tactical requirements. Through this assessment, it is possible to determine the parameters of components and devices installed on the Aerial target.
References
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http://www.braeunig.us/space/aerodyn_wip.htm, truy cập ngày 29/5/2021.
