Performance and Weight Parameters Calculation for Hydrogen- and Battery-Powered Aircraft Concepts
This article describes the creation of a program that would be useful for calculating mathematical models in order to estimate the weight of aircraft components. Using several parameters, it can calculate other parameters of civil transport aircraft powered by batteries or fuel cells. The main goals...
Main Authors: | Michal Janovec, Viktor Babčan, Branislav Kandera, Kristína Šajbanová, Filip Škultéty, Ľuboš Halvoň |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-05-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/5/482 |
Similar Items
-
Design of Batteries for a Hybrid Propulsion System of a Training Aircraft
by: Michal Janovec, et al.
Published: (2021-12-01) -
Energy Conversion System and Control of Fuel-Cell and Battery-Based Hybrid Drive for Light Aircraft
by: Tomasz Miazga, et al.
Published: (2021-02-01) -
Performance and Emission of the Aircraft with Hybrid Propulsion During Take-Off Operation Cycle
by: Małgorzata Pawlak, et al.
Published: (2024-02-01) -
Parametric Analysis for Hybrid–Electric Regional Aircraft Conceptual Design and Development
by: Giuseppe Palaia, et al.
Published: (2023-10-01) -
Noise Impact Assessment of UAS Operation in Urbanised Areas: Field Measurements and a Simulation
by: Filip Škultéty, et al.
Published: (2023-05-01)