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- Article name
- THE TECHNIQUE OF CALCULATION ESTIMATES THE MAXIMUM ALLOWABLE TAKE-OFF WEIGHT OF UNMANNED AIRCRAFT AS THE DESIGN STAGE
- Authors
- Eryomin E. M., , gniiivm-k@yandex.ru, State Flight Test Center Chkalov, Akhtubinsk, Russia
Russkin A. V., , tx97@mail.ru, Academy of Civil Defense of EMERCOM of Russia, Khimki, Moscow region, Russia
- Keywords
- design of unmanned aerial vehicles / takeoff weight / the weight calculation / the shape of the unmanned aerial vehicles
- Year
- 2014 Issue 1 Pages 39 - 42
- Code EDN
- Code DOI
- Abstract
- Discloses a method of calculating the indicative weigth UAV aircraft type small and medium range in weigth from 15 to 150 kg as the design state, allowing it to adequately assess the maximum allowable takeoff weigth, depending on the set values and duration of the payload mass.
- Text
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