Synthesis of design and technological solutions in the development of UAV launch system
Keywords:
unmanned aerial vehicles, solid-fuel, rocket engine, launch, manufacturabilityAbstract
This scientific paper examines the process of launching unmanned aerial vehicles (UAVs) using a solid-fuel rocket engine. The primary focus is on analyzing the design and technological aspects and advantages of using solid-fuel rocket engines for UAV launches, as well as describing the design features and technical characteristics of such systems. The study includes an analysis of the current state of UAV development, the challenges of UAV launch, and modern trends in launch system design. It addresses issues of reliability and safety in using solid fuel, as well as the impact of various parameters on launch efficiency. An analysis of possible UAV design schemes with rocket-assisted launch methods is conducted, comparing them with other launch systems. Examples of implemented systems are provided, and the feasibility of using the proposed technical solutions in them is analyzed. Constructive and technological solutions that meet the criteria of manufacturability, reliability, and resource efficiency are proposed. The feasibility and practicality of using the proposed design and technological solutions for UAV launch tasks are assessed, taking into account the aforementioned criteria and conducting a comparative analysis with previously considered launch schemes and systems. The potential use of such systems for military and civilian purposes, their adaptability to different operating conditions, and possible economic benefits are separately analyzed. Based on the obtained data, conclusions are drawn regarding the prospects for the development of this technology and recommendations for further research. Specifically, the influence of climatic conditions and other external factors on the reliability of UAV launches using solid-fuel rocket engines is considered, as well as possible ways to optimize designs to improve efficiency.
Downloads
References
Даник, Ю. Г. (2008). Безпілотні літальні апарати: означення. Класифікація, стан та перспективи розвитку і використання. Ко-смічна наука і технологія, 1, 30-43.
Осипов, Ю. М., & Орлов, С. В. (2015). Старт лёгких беспи-лотных летательных аппаратов. Системи озброєння і військова техніка, (3), 116-119.
Довбиш, І. О., Муравйов, О. В., Галаган, Р. М., Богдан, Г. А., & Момот, А. С. (2023). Силові установки та джерела енергії сучасних БПЛА.
Фокус, Р. (2023, 13 лютого). Десятая "Лелека-100" отпра-вилась бить оккупантов: на что способен наш БПЛА (видео). ФОКУС. https://focus.ua/digital/549667-desyataya-leleka-100-otpravilas-bit-okkupantov-na-chto-sposoben-nash-bpla-video
Ukrinform. (2023, 27 жовтня). Безпілотник Bayraktar TB3 пройшов тест на швидкість руху. Укрінформ - актуальні новини України та світу. https://www.ukrinform.ua/rubric-technology/3779405-bezpilotnik-bayraktar-tb3-projsov-test-na-svidkist-ruhu.html
Середа, В. (2010). Класифікація законів розподілу тяги зу-силля наземних пускових установок безпілотних літальних апара-тів. Авіаційно-космічна техніка и технологія, 4(71), 63–66.
Andrei, I. C., Stroe, G. L., Berbente, S., Prisacariu, V., Costea, E., Popescu, I., & Ioan, O. (2023). Risk management applied to aerospace engineering design. ISSN, ISSN-L: 2247-3173, 113.
Ту-141 "Стриж" Defense Express. (2023, 7 лютого). Війсь-ковий портал Defense Express - все про військову справу. https://defence-ua.com/weapon_and_tech/ostatochno_pidtverdzheno_zsu_z_arhajichnih_tu_141_strizh_zrobili_zbrojeju_dlja_udariv_po_objektam_bilja_moskvi-10559.html
Залата, О. (2023, 21 серпня). "Бобри" замість ракет: які небезпечні ударні дрони має Україна і на що вони здатні (відео). ФОКУС. https://focus.ua/uk/digital/587087-bobri-zamist-raket-yaki-nebezpechni-udarni-droni-maye-ukrajina-i-na-shcho-voni-zdatni-video
Downloads
Published
Issue
Section
License
Copyright (c) 2024 Артем Швець, Ігор Білоцерковський, Олексій Кулик, Олександр Добродомов (Автор)
![Creative Commons License](http://i.creativecommons.org/l/by/4.0/88x31.png)
This work is licensed under a Creative Commons Attribution 4.0 International License.
All articles published in the journal Challenges and Issues of Modern Science are licensed under the Creative Commons Attribution 4.0 International (CC BY) license. This means that you are free to:
- Share, copy, and redistribute the article in any medium or format
- Adapt, remix, transform, and build upon the article
as long as you provide appropriate credit to the original work, include the authors' names, article title, journal name, and indicate that the work is licensed under CC BY. Any use of the material should not imply endorsement by the authors or the journal.