DESIGN PARAMETERS OF VERTICAL TAKE-OFF AIRCRAFT

Authors

  • U. Kassymov Department of Space Engineering and Technology, ENU named after L. Gumilyov
  • V. Dzhundibayev Department of Space Engineering and Technology, L. Gumilyov ENU
  • M. Kassabekov Department of Mechanics of L. Gumilyov ENU
  • K. Akhmetov Department of Space Engineering and Technology, L. Gumilyov ENU

Keywords:

aircraft, engine, battery, body, control system

Abstract

The article presents the technical features of a new type of ultralight aircraft. This aircraft was developed in a draft version by Special Design and Technological Bureau Aerospace and Special Engineering LLP, Satpayeva 5, Nur-Sultan, Kazakhstan. In recent years, worldwide interest in small vertical take-off and landing vehicles has sharply increased, which have obvious advantages over other types of vehicles. These devices have high mobility, low cost and availability to a large number of consumers. Electrical versions of these devices will help solve the environmental problem and improve the transport situation in large cities.

Author Biographies

U. Kassymov , Department of Space Engineering and Technology, ENU named after L. Gumilyov

PhD, Professor

V. Dzhundibayev , Department of Space Engineering and Technology, L. Gumilyov ENU

PhD, Professor

M. Kassabekov , Department of Mechanics of L. Gumilyov ENU

PhD, Professor

K. Akhmetov, Department of Space Engineering and Technology, L. Gumilyov ENU

PhD, Head of the Department

References

U.Kassymov "Multi-cycle fatigue strength of bearing structure materials of mechanical equipment automatic installations, Monograph, "Master software", Astana, 2013,

U.Kassymov. Fundamentals of ultralight aircraft design. Monograph, "Master PO", Astana, 2017, 184 p.

U.Kassymov, S Otegali, M. Amangaliev, N. Kassymov. Calculation and design of multifunctional aircraft. Monograph. "Master PO", Astana, 2018

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Published

2021-11-30

Issue

Vol. 1 No. 55 (2021)

Section

Статьи

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