Mathematical model of pneumatic launch system with effect of unmanned aerial vehicle, engine and propeller characteristics

Mathematical model of pneumatic launch system with effect of unmanned aerial vehicle, engine and propeller characteristics

Despite significant progress in the development of modern unmanned aerial vehicles (UAVs), universal launch systems are not currently used for them. In fact, each UAV project requires its own launcher, which is inefficient in many cases. To evaluate the characteristics of UAV launchers, simple metho...

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Bibliographic Details
Main Author: Olexander Khrulev
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2023-08-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
бпла
стартовий комплекс
катапульта
поршневий двигун
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/2055

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