Estimation of the take-off weight of a combat helicopter with specified performance on the basis of the existence equation | Tarasov | Civil Aviation High Technologies

Civil Aviation High Technologies
Nauchnyi Vestnik MGTU GA

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

eng | рус

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Tarasov A.L., Prozorov M.A. Estimation of the take-off weight of a combat helicopter with specified performance on the basis of the existence equation. Civil Aviation High Technologies. 2024;27(5):90-102. (In Russ.) https://doi.org/10.26467/2079-0619-2024-27-5-90-102

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

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Eliseev B.P.

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About the Authors

A. L. Tarasov
Branch of the Russian Air Force Military Educational and Scientific Centre Zhukovsky – Gagarin Air Force Academy
Russian Federation

Andrey L. Tarasov, Candidate of Technical Sciences, Associate Professor, the Head of the Department of Helicopter Design and Operation and Engines,

Syzran.

M. A. Prozorov
Branch of the Russian Air Force Military Educational and Scientific Centre Zhukovsky – Gagarin Air Force Academy
Russian Federation

Michael A. Prozorov, Senior Lecturer, the Department of Helicopter Design and Operation and Engines,

Syzran.

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