Modeling the Overall, Mass and Aerodynamic Characteristics of the First and Second Stages of the System for Launching Micro- and Nanosatellites into Low Earth Orbits
Transport Means 2021: Proceedings of the 25th International Scientific Conference 2021
Nikolajs Kuļešovs, Sergey Kravchenko, Vladimirs Šestakovs, Ilmārs Blumbergs, Dmitrijs Titovs, Natalia Panova

The Riga Technical University (RTU) is developing a system for launching pico- and nanosatellites into low Earth orbits (LEO). The system as a platform includes the transport aircraft A319 and a three-stage launching system with the code name LatLaunch. One of the supersonic fighters was selected as the LatLaunch aerodynamic prototype based on its technical characteristics (flight altitude record, flight speed record, and information availability on some aircraft aerodynamic characteristics). The article presents the results of modeling the aerodynamic characteristics of the first and the second stages of the LatLaunch system, represented by modeling using 3D modeling of SolidWorks software and Scilab at subsonic, transonic, supersonic, and low hypersonic flight speed modes of LatLaunch flight.


Keywords
a platform aircraft, a satellite launch system, aerodynamic characteristics, mathematical modelling
Hyperlink
https://transportmeans.ktu.edu/wp-content/uploads/sites/307/2018/02/Transport-Means-2021-Part-II.pdf

Kuļešovs, N., Kravchenko, S., Šestakovs, V., Blumbergs, I., Titovs, D., Panova, N. Modeling the Overall, Mass and Aerodynamic Characteristics of the First and Second Stages of the System for Launching Micro- and Nanosatellites into Low Earth Orbits. In: Transport Means 2021: Proceedings of the 25th International Scientific Conference, Lithuania, Kaunas, 6-8 October, 2021. Kaunas: Kaunas University of Technology, 2021, pp.555-561. ISSN 1822-296X. e-ISSN 2351-7034.

Publication language
English (en)
The Scientific Library of the Riga Technical University.
E-mail: uzzinas@rtu.lv; Phone: +371 28399196