Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system

The article discusses a method for calculating, as a first approximation, the take-off weight of a light aircraft with a hybrid power plant based on piston and electric engines. A brief overview of organizations dealing with hybrid power plants is given. The influence of the degree of hybridization...

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Bibliographic Details
Published in:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Main Authors: A. V. Sychev, I. V. Arbuzov, Yu. A. Ravikovich
Format: Article
Language:English
Published: Samara National Research University 2024-07-01
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/27656/10659