Reliability assessment of convertible aircraft with hybrid propulsion system and multirotor lifting system

A. V. Redkin; Yu. A. Yaloza; I. E. Kovalev

Civil Aviation High Technologies
Nauchnyi Vestnik MGTU GA

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Redkin A.V., Yaloza Yu.A., Kovalev I.E. Reliability assessment of convertible aircraft with hybrid propulsion system and multirotor lifting system. Civil Aviation High Technologies. 2020;23(5):76-96. (In Russ.) https://doi.org/10.26467/2079-0619-2020-23-5-76-96

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This work is licensed under a Creative Commons Attribution 4.0 License.

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Eliseev B.P.

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About the Authors

A. V. Redkin
FSUE Central Aerohydrodynamic Institute
Russian Federation

Zhukovsky

Yu. A. Yaloza
Gromov Flight Research Institute Zhukovsky; Moscow Aviation Institute, Branch "Strela"
Russian Federation

Yuri A. Yaloza, Candidate of Technical Sciences, Head of the Laboratory; Associate Professor of Design and Construction of Aircraft and Experimental Installation Chair (C-11)

Zhukovsky

I. E. Kovalev
FSUE Central Aerohydrodynamic Institute
Russian Federation

Igor E. Kovalev, Doctor of Technical Sciences, Professor

Zhukovsky