Design and construction of the army unmanned aerial vehicle with a new generation launch system «RPSKD-2»

Abstract

The scientific article presents the design and construction of a two-case army unmanned aerial vehicle with a launch system of a new generation «RPSKD-2», which can be used for combat purposes. The study lists the main design units of the launch system, army unmanned aerial vehicle and cases. The combat equipment of the RPSKD-2 UAV provides for suspended armed cases that will be attached to the lower part. When designing and constructing an army UAV, foreign and domestic experience in machine-building production in this field of knowledge was studied. When modeling the UAV, the Compass and Siemens NX software product was used. The following general scientific methods for studying research materials were used in the article: analysis, deduction and modeling. The purpose of the study is to develop a two-case UAV with a launch system. This article is the first part of the study, in a number of author's scientific articles. Further publications of the authors will be devoted to the UAV structural and functional control system, which includes: telemetry, gyroscopes, automatic control system, sensors, controllers, engine, etc.